CA2425179A1 - Inorganic matrix compositions and composites incorporating the matrix composition - Google Patents
Inorganic matrix compositions and composites incorporating the matrix composition Download PDFInfo
- Publication number
- CA2425179A1 CA2425179A1 CA002425179A CA2425179A CA2425179A1 CA 2425179 A1 CA2425179 A1 CA 2425179A1 CA 002425179 A CA002425179 A CA 002425179A CA 2425179 A CA2425179 A CA 2425179A CA 2425179 A1 CA2425179 A1 CA 2425179A1
- Authority
- CA
- Canada
- Prior art keywords
- composition
- glass
- fibers
- alkali
- group
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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- 239000000203 mixture Substances 0.000 title claims abstract description 161
- 239000002131 composite material Substances 0.000 title claims abstract description 75
- 239000011159 matrix material Substances 0.000 title claims abstract description 51
- 239000011521 glass Substances 0.000 claims abstract description 132
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 91
- 230000002378 acidificating effect Effects 0.000 claims abstract description 52
- 238000000034 method Methods 0.000 claims abstract description 48
- 229910001868 water Inorganic materials 0.000 claims abstract description 48
- 229910052910 alkali metal silicate Inorganic materials 0.000 claims abstract description 46
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 45
- 239000000945 filler Substances 0.000 claims abstract description 36
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 32
- 239000011347 resin Substances 0.000 claims abstract description 30
- 229920005989 resin Polymers 0.000 claims abstract description 30
- 229910052681 coesite Inorganic materials 0.000 claims abstract description 20
- 229910052906 cristobalite Inorganic materials 0.000 claims abstract description 20
- 229910052682 stishovite Inorganic materials 0.000 claims abstract description 20
- 229910052905 tridymite Inorganic materials 0.000 claims abstract description 20
- 235000012239 silicon dioxide Nutrition 0.000 claims abstract description 17
- 229910001854 alkali hydroxide Inorganic materials 0.000 claims abstract description 13
- 150000008044 alkali metal hydroxides Chemical class 0.000 claims abstract description 13
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 13
- 239000002243 precursor Substances 0.000 claims abstract description 12
- 238000004519 manufacturing process Methods 0.000 claims abstract description 9
- 239000002002 slurry Substances 0.000 claims abstract description 9
- 238000000748 compression moulding Methods 0.000 claims abstract description 4
- 239000000835 fiber Substances 0.000 claims description 47
- 239000000463 material Substances 0.000 claims description 43
- 230000008569 process Effects 0.000 claims description 30
- 238000012545 processing Methods 0.000 claims description 27
- 239000003365 glass fiber Substances 0.000 claims description 25
- 239000000843 powder Substances 0.000 claims description 23
- 239000000243 solution Substances 0.000 claims description 21
- 239000011230 binding agent Substances 0.000 claims description 20
- KWYUFKZDYYNOTN-UHFFFAOYSA-M Potassium hydroxide Chemical compound [OH-].[K+] KWYUFKZDYYNOTN-UHFFFAOYSA-M 0.000 claims description 19
- 239000000919 ceramic Substances 0.000 claims description 19
- 230000002787 reinforcement Effects 0.000 claims description 19
- 239000004927 clay Substances 0.000 claims description 17
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 claims description 17
- -1 spheres Substances 0.000 claims description 15
- 239000003607 modifier Substances 0.000 claims description 14
- 239000005995 Aluminium silicate Substances 0.000 claims description 13
- 239000003513 alkali Substances 0.000 claims description 13
- 235000012211 aluminium silicate Nutrition 0.000 claims description 13
- 229910052751 metal Inorganic materials 0.000 claims description 12
- 239000002184 metal Substances 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- 229910021487 silica fume Inorganic materials 0.000 claims description 10
- 238000000465 moulding Methods 0.000 claims description 9
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 239000007795 chemical reaction product Substances 0.000 claims description 8
- 239000000499 gel Substances 0.000 claims description 8
- 239000011777 magnesium Substances 0.000 claims description 8
- 239000005365 phosphate glass Substances 0.000 claims description 8
- 229910052698 phosphorus Inorganic materials 0.000 claims description 8
- 239000011574 phosphorus Substances 0.000 claims description 8
- 239000010453 quartz Substances 0.000 claims description 8
- 229910052710 silicon Inorganic materials 0.000 claims description 8
- 239000010703 silicon Substances 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 8
- 239000010936 titanium Substances 0.000 claims description 8
- 239000011701 zinc Substances 0.000 claims description 8
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 7
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 7
- 229910052788 barium Inorganic materials 0.000 claims description 7
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 claims description 7
- 229910052796 boron Inorganic materials 0.000 claims description 7
- 229920000592 inorganic polymer Polymers 0.000 claims description 7
- 239000007788 liquid Substances 0.000 claims description 7
- 229910052749 magnesium Inorganic materials 0.000 claims description 7
- 150000007530 organic bases Chemical class 0.000 claims description 7
- 235000019353 potassium silicate Nutrition 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 7
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 6
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 claims description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 6
- 239000004917 carbon fiber Substances 0.000 claims description 6
- 229910052744 lithium Inorganic materials 0.000 claims description 6
- 229910052725 zinc Inorganic materials 0.000 claims description 6
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- 229910052779 Neodymium Inorganic materials 0.000 claims description 5
- 239000004111 Potassium silicate Substances 0.000 claims description 5
- 239000004115 Sodium Silicate Substances 0.000 claims description 5
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 5
- 229910052791 calcium Inorganic materials 0.000 claims description 5
- 239000011575 calcium Substances 0.000 claims description 5
- 229910052746 lanthanum Inorganic materials 0.000 claims description 5
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 5
- 239000005300 metallic glass Substances 0.000 claims description 5
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims description 5
- 150000007524 organic acids Chemical group 0.000 claims description 5
- 239000011368 organic material Substances 0.000 claims description 5
- 239000002245 particle Substances 0.000 claims description 5
- NNHHDJVEYQHLHG-UHFFFAOYSA-N potassium silicate Chemical group [K+].[K+].[O-][Si]([O-])=O NNHHDJVEYQHLHG-UHFFFAOYSA-N 0.000 claims description 5
- 229910052913 potassium silicate Inorganic materials 0.000 claims description 5
- 239000011734 sodium Substances 0.000 claims description 5
- 229910052717 sulfur Inorganic materials 0.000 claims description 5
- 239000011593 sulfur Substances 0.000 claims description 5
- 229910052684 Cerium Inorganic materials 0.000 claims description 4
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 claims description 4
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 claims description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 4
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 claims description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 4
- 150000001450 anions Chemical class 0.000 claims description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 150000001768 cations Chemical class 0.000 claims description 4
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 claims description 4
- 229910052733 gallium Inorganic materials 0.000 claims description 4
- 238000001802 infusion Methods 0.000 claims description 4
- 229910052909 inorganic silicate Inorganic materials 0.000 claims description 4
- 229910052760 oxygen Inorganic materials 0.000 claims description 4
- 239000001301 oxygen Substances 0.000 claims description 4
- 229910052708 sodium Inorganic materials 0.000 claims description 4
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 claims description 4
- 229910052911 sodium silicate Inorganic materials 0.000 claims description 4
- 229910052712 strontium Inorganic materials 0.000 claims description 4
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims description 4
- 229910052727 yttrium Inorganic materials 0.000 claims description 4
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- 229920002748 Basalt fiber Polymers 0.000 claims description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- FUJCRWPEOMXPAD-UHFFFAOYSA-N Li2O Inorganic materials [Li+].[Li+].[O-2] FUJCRWPEOMXPAD-UHFFFAOYSA-N 0.000 claims description 3
- 229920000914 Metallic fiber Polymers 0.000 claims description 3
- 229910000990 Ni alloy Inorganic materials 0.000 claims description 3
- 229910052775 Thulium Inorganic materials 0.000 claims description 3
- SMWDFEZZVXVKRB-UHFFFAOYSA-N anhydrous quinoline Natural products N1=CC=CC2=CC=CC=C21 SMWDFEZZVXVKRB-UHFFFAOYSA-N 0.000 claims description 3
- 239000004760 aramid Substances 0.000 claims description 3
- 229920006231 aramid fiber Polymers 0.000 claims description 3
- 229910052793 cadmium Inorganic materials 0.000 claims description 3
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims description 3
- 150000004770 chalcogenides Chemical class 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 229920001971 elastomer Polymers 0.000 claims description 3
- 238000001879 gelation Methods 0.000 claims description 3
- 239000010439 graphite Substances 0.000 claims description 3
- 229910002804 graphite Inorganic materials 0.000 claims description 3
- 125000005843 halogen group Chemical group 0.000 claims description 3
- 229910052500 inorganic mineral Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 3
- 239000011707 mineral Substances 0.000 claims description 3
- 229910052700 potassium Inorganic materials 0.000 claims description 3
- 239000011591 potassium Substances 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 3
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 claims description 2
- 239000004412 Bulk moulding compound Substances 0.000 claims description 2
- 229910052692 Dysprosium Inorganic materials 0.000 claims description 2
- 229910052691 Erbium Inorganic materials 0.000 claims description 2
- 229910052693 Europium Inorganic materials 0.000 claims description 2
- PXGOKWXKJXAPGV-UHFFFAOYSA-N Fluorine Chemical compound FF PXGOKWXKJXAPGV-UHFFFAOYSA-N 0.000 claims description 2
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 2
- 229910052689 Holmium Inorganic materials 0.000 claims description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 2
- 229910052772 Samarium Inorganic materials 0.000 claims description 2
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 claims description 2
- 239000003677 Sheet moulding compound Substances 0.000 claims description 2
- QAOWNCQODCNURD-UHFFFAOYSA-L Sulfate Chemical compound [O-]S([O-])(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-L 0.000 claims description 2
- 229910052771 Terbium Inorganic materials 0.000 claims description 2
- 229910052776 Thorium Inorganic materials 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- 229910052770 Uranium Inorganic materials 0.000 claims description 2
- 229910052769 Ytterbium Inorganic materials 0.000 claims description 2
- 229910052767 actinium Inorganic materials 0.000 claims description 2
- QQINRWTZWGJFDB-UHFFFAOYSA-N actinium atom Chemical compound [Ac] QQINRWTZWGJFDB-UHFFFAOYSA-N 0.000 claims description 2
- 229910052787 antimony Inorganic materials 0.000 claims description 2
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 2
- 229910052785 arsenic Inorganic materials 0.000 claims description 2
- RQNWIZPPADIBDY-UHFFFAOYSA-N arsenic atom Chemical compound [As] RQNWIZPPADIBDY-UHFFFAOYSA-N 0.000 claims description 2
- 229910052792 caesium Inorganic materials 0.000 claims description 2
- TVFDJXOCXUVLDH-UHFFFAOYSA-N caesium atom Chemical compound [Cs] TVFDJXOCXUVLDH-UHFFFAOYSA-N 0.000 claims description 2
- 238000005266 casting Methods 0.000 claims description 2
- 229910017052 cobalt Inorganic materials 0.000 claims description 2
- 239000010941 cobalt Substances 0.000 claims description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 2
- 239000008119 colloidal silica Substances 0.000 claims description 2
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 claims description 2
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 claims description 2
- 239000000806 elastomer Substances 0.000 claims description 2
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 claims description 2
- OGPBJKLSAFTDLK-UHFFFAOYSA-N europium atom Chemical compound [Eu] OGPBJKLSAFTDLK-UHFFFAOYSA-N 0.000 claims description 2
- 238000001125 extrusion Methods 0.000 claims description 2
- 238000009730 filament winding Methods 0.000 claims description 2
- 235000013312 flour Nutrition 0.000 claims description 2
- 239000011737 fluorine Substances 0.000 claims description 2
- 229910052731 fluorine Inorganic materials 0.000 claims description 2
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 2
- 229910052732 germanium Inorganic materials 0.000 claims description 2
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 claims description 2
- KJZYNXUDTRRSPN-UHFFFAOYSA-N holmium atom Chemical compound [Ho] KJZYNXUDTRRSPN-UHFFFAOYSA-N 0.000 claims description 2
- 238000001746 injection moulding Methods 0.000 claims description 2
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 claims description 2
- 229910052753 mercury Inorganic materials 0.000 claims description 2
- 239000010445 mica Substances 0.000 claims description 2
- 229910052618 mica group Inorganic materials 0.000 claims description 2
- 239000004005 microsphere Substances 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 239000011733 molybdenum Substances 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- 150000003222 pyridines Chemical class 0.000 claims description 2
- 229910052701 rubidium Inorganic materials 0.000 claims description 2
- IGLNJRXAVVLDKE-UHFFFAOYSA-N rubidium atom Chemical compound [Rb] IGLNJRXAVVLDKE-UHFFFAOYSA-N 0.000 claims description 2
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 claims description 2
- 239000004576 sand Substances 0.000 claims description 2
- 229910052711 selenium Inorganic materials 0.000 claims description 2
- 239000011669 selenium Substances 0.000 claims description 2
- 238000004528 spin coating Methods 0.000 claims description 2
- 229910052714 tellurium Inorganic materials 0.000 claims description 2
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 claims description 2
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 claims description 2
- 229910052718 tin Inorganic materials 0.000 claims description 2
- 238000001721 transfer moulding Methods 0.000 claims description 2
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 claims description 2
- 238000009755 vacuum infusion Methods 0.000 claims description 2
- 239000010455 vermiculite Substances 0.000 claims description 2
- 229910052902 vermiculite Inorganic materials 0.000 claims description 2
- 235000019354 vermiculite Nutrition 0.000 claims description 2
- 238000009756 wet lay-up Methods 0.000 claims description 2
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 claims description 2
- 239000004698 Polyethylene Substances 0.000 claims 2
- 239000002557 mineral fiber Substances 0.000 claims 2
- 229920000573 polyethylene Polymers 0.000 claims 2
- 239000000725 suspension Substances 0.000 claims 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims 1
- 229910052777 Praseodymium Inorganic materials 0.000 claims 1
- 229910021486 amorphous silicon dioxide Inorganic materials 0.000 claims 1
- 229910052797 bismuth Inorganic materials 0.000 claims 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims 1
- 239000005385 borate glass Substances 0.000 claims 1
- 229910052804 chromium Inorganic materials 0.000 claims 1
- 239000011651 chromium Substances 0.000 claims 1
- 229910021488 crystalline silicon dioxide Inorganic materials 0.000 claims 1
- XUCJHNOBJLKZNU-UHFFFAOYSA-M dilithium;hydroxide Chemical compound [Li+].[Li+].[OH-] XUCJHNOBJLKZNU-UHFFFAOYSA-M 0.000 claims 1
- 229910021485 fumed silica Inorganic materials 0.000 claims 1
- 229910010272 inorganic material Inorganic materials 0.000 claims 1
- 239000011147 inorganic material Substances 0.000 claims 1
- 239000011133 lead Substances 0.000 claims 1
- 229910052757 nitrogen Inorganic materials 0.000 claims 1
- IJGRMHOSHXDMSA-UHFFFAOYSA-N nitrogen Substances N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims 1
- 125000004430 oxygen atom Chemical group O* 0.000 claims 1
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims 1
- JUJWROOIHBZHMG-UHFFFAOYSA-N pyridine Substances C1=CC=NC=C1 JUJWROOIHBZHMG-UHFFFAOYSA-N 0.000 claims 1
- UMJSCPRVCHMLSP-UHFFFAOYSA-N pyridine Natural products COC1=CC=CN=C1 UMJSCPRVCHMLSP-UHFFFAOYSA-N 0.000 claims 1
- 125000002943 quinolinyl group Chemical group N1=C(C=CC2=CC=CC=C12)* 0.000 claims 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims 1
- 229910052721 tungsten Inorganic materials 0.000 claims 1
- 239000010937 tungsten Substances 0.000 claims 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 abstract description 11
- 239000000654 additive Substances 0.000 abstract description 10
- 229920000620 organic polymer Polymers 0.000 abstract description 9
- 238000010094 polymer processing Methods 0.000 abstract description 3
- 239000006057 Non-nutritive feed additive Substances 0.000 abstract 1
- 238000009472 formulation Methods 0.000 description 29
- 239000004744 fabric Substances 0.000 description 19
- 238000002156 mixing Methods 0.000 description 11
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 10
- 150000001875 compounds Chemical class 0.000 description 8
- 150000002739 metals Chemical class 0.000 description 8
- 239000000047 product Substances 0.000 description 8
- 239000000395 magnesium oxide Substances 0.000 description 7
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 7
- 238000003756 stirring Methods 0.000 description 7
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 6
- 239000002585 base Substances 0.000 description 6
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 description 6
- 235000010338 boric acid Nutrition 0.000 description 6
- 239000011153 ceramic matrix composite Substances 0.000 description 6
- 229920000642 polymer Polymers 0.000 description 6
- 230000009257 reactivity Effects 0.000 description 6
- 239000000779 smoke Substances 0.000 description 6
- 229910019142 PO4 Inorganic materials 0.000 description 5
- 229910000272 alkali metal oxide Inorganic materials 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- 230000003301 hydrolyzing effect Effects 0.000 description 5
- 238000005470 impregnation Methods 0.000 description 5
- 239000011156 metal matrix composite Substances 0.000 description 5
- 239000010452 phosphate Substances 0.000 description 5
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 5
- 230000000704 physical effect Effects 0.000 description 5
- 238000007670 refining Methods 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 4
- 239000004615 ingredient Substances 0.000 description 4
- 239000012212 insulator Substances 0.000 description 4
- JVTAAEKCZFNVCJ-UHFFFAOYSA-N lactic acid Chemical compound CC(O)C(O)=O JVTAAEKCZFNVCJ-UHFFFAOYSA-N 0.000 description 4
- 230000007935 neutral effect Effects 0.000 description 4
- 239000012783 reinforcing fiber Substances 0.000 description 4
- 150000004760 silicates Chemical class 0.000 description 4
- 229910010271 silicon carbide Inorganic materials 0.000 description 4
- 229910015444 B(OH)3 Inorganic materials 0.000 description 3
- KKCBUQHMOMHUOY-UHFFFAOYSA-N Na2O Inorganic materials [O-2].[Na+].[Na+] KKCBUQHMOMHUOY-UHFFFAOYSA-N 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 239000004327 boric acid Substances 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000006482 condensation reaction Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 239000011256 inorganic filler Substances 0.000 description 3
- 229910003475 inorganic filler Inorganic materials 0.000 description 3
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 239000000376 reactant Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- BTBUEUYNUDRHOZ-UHFFFAOYSA-N Borate Chemical compound [O-]B([O-])[O-] BTBUEUYNUDRHOZ-UHFFFAOYSA-N 0.000 description 2
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 2
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 244000309464 bull Species 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000007596 consolidation process Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000006378 damage Effects 0.000 description 2
- 238000004090 dissolution Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 150000001261 hydroxy acids Chemical class 0.000 description 2
- 239000003112 inhibitor Substances 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 239000004310 lactic acid Substances 0.000 description 2
- 235000014655 lactic acid Nutrition 0.000 description 2
- 229910052808 lithium carbonate Inorganic materials 0.000 description 2
- YIXJRHPUWRPCBB-UHFFFAOYSA-N magnesium nitrate Chemical compound [Mg+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O YIXJRHPUWRPCBB-UHFFFAOYSA-N 0.000 description 2
- 229910044991 metal oxide Inorganic materials 0.000 description 2
- 150000004706 metal oxides Chemical class 0.000 description 2
- 235000010755 mineral Nutrition 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000006060 molten glass Substances 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- CHWRSCGUEQEHOH-UHFFFAOYSA-N potassium oxide Chemical compound [O-2].[K+].[K+] CHWRSCGUEQEHOH-UHFFFAOYSA-N 0.000 description 2
- 229910001950 potassium oxide Inorganic materials 0.000 description 2
- 230000000135 prohibitive effect Effects 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 229910002027 silica gel Inorganic materials 0.000 description 2
- 239000000741 silica gel Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 235000019351 sodium silicates Nutrition 0.000 description 2
- 241000894007 species Species 0.000 description 2
- 230000001988 toxicity Effects 0.000 description 2
- 231100000419 toxicity Toxicity 0.000 description 2
- RNFJDJUURJAICM-UHFFFAOYSA-N 2,2,4,4,6,6-hexaphenoxy-1,3,5-triaza-2$l^{5},4$l^{5},6$l^{5}-triphosphacyclohexa-1,3,5-triene Chemical compound N=1P(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP=1(OC=1C=CC=CC=1)OC1=CC=CC=C1 RNFJDJUURJAICM-UHFFFAOYSA-N 0.000 description 1
- RZVAJINKPMORJF-UHFFFAOYSA-N Acetaminophen Chemical compound CC(=O)NC1=CC=C(O)C=C1 RZVAJINKPMORJF-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- 239000004971 Cross linker Substances 0.000 description 1
- 239000004594 Masterbatch (MB) Substances 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- CYTYCFOTNPOANT-UHFFFAOYSA-N Perchloroethylene Chemical compound ClC(Cl)=C(Cl)Cl CYTYCFOTNPOANT-UHFFFAOYSA-N 0.000 description 1
- 239000004642 Polyimide Substances 0.000 description 1
- 229910020169 SiOa Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- IUHFWCGCSVTMPG-UHFFFAOYSA-N [C].[C] Chemical class [C].[C] IUHFWCGCSVTMPG-UHFFFAOYSA-N 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 229910052768 actinide Inorganic materials 0.000 description 1
- 150000001255 actinides Chemical class 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910000287 alkaline earth metal oxide Inorganic materials 0.000 description 1
- 150000004645 aluminates Chemical class 0.000 description 1
- LFVGISIMTYGQHF-UHFFFAOYSA-N ammonium dihydrogen phosphate Chemical compound [NH4+].OP(O)([O-])=O LFVGISIMTYGQHF-UHFFFAOYSA-N 0.000 description 1
- 229940111121 antirheumatic drug quinolines Drugs 0.000 description 1
- AYJRCSIUFZENHW-UHFFFAOYSA-L barium carbonate Inorganic materials [Ba+2].[O-]C([O-])=O AYJRCSIUFZENHW-UHFFFAOYSA-L 0.000 description 1
- 239000005388 borosilicate glass Substances 0.000 description 1
- 239000013590 bulk material Substances 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 150000001767 cationic compounds Chemical class 0.000 description 1
- 239000003518 caustics Substances 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 239000004567 concrete Substances 0.000 description 1
- 239000011231 conductive filler Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- MNNHAPBLZZVQHP-UHFFFAOYSA-N diammonium hydrogen phosphate Chemical compound [NH4+].[NH4+].OP([O-])([O-])=O MNNHAPBLZZVQHP-UHFFFAOYSA-N 0.000 description 1
- 238000000113 differential scanning calorimetry Methods 0.000 description 1
- ZPWVASYFFYYZEW-UHFFFAOYSA-L dipotassium hydrogen phosphate Chemical compound [K+].[K+].OP([O-])([O-])=O ZPWVASYFFYYZEW-UHFFFAOYSA-L 0.000 description 1
- 229910000396 dipotassium phosphate Inorganic materials 0.000 description 1
- 235000019797 dipotassium phosphate Nutrition 0.000 description 1
- 238000002845 discoloration Methods 0.000 description 1
- BNIILDVGGAEEIG-UHFFFAOYSA-L disodium hydrogen phosphate Chemical compound [Na+].[Na+].OP([O-])([O-])=O BNIILDVGGAEEIG-UHFFFAOYSA-L 0.000 description 1
- 230000035622 drinking Effects 0.000 description 1
- 238000010292 electrical insulation Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 210000003195 fascia Anatomy 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000003063 flame retardant Substances 0.000 description 1
- 238000005187 foaming Methods 0.000 description 1
- 238000005816 glass manufacturing process Methods 0.000 description 1
- 230000009477 glass transition Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052736 halogen Chemical group 0.000 description 1
- 150000002367 halogens Chemical group 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000010954 inorganic particle Substances 0.000 description 1
- 229910052747 lanthanoid Inorganic materials 0.000 description 1
- 150000002602 lanthanoids Chemical class 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000012764 mineral filler Substances 0.000 description 1
- 229910000403 monosodium phosphate Inorganic materials 0.000 description 1
- 235000019799 monosodium phosphate Nutrition 0.000 description 1
- 229910052901 montmorillonite Inorganic materials 0.000 description 1
- 230000003472 neutralizing effect Effects 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000005304 optical glass Substances 0.000 description 1
- 235000005985 organic acids Nutrition 0.000 description 1
- 239000012766 organic filler Substances 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229940072033 potash Drugs 0.000 description 1
- BWHMMNNQKKPAPP-UHFFFAOYSA-L potassium carbonate Substances [K+].[K+].[O-]C([O-])=O BWHMMNNQKKPAPP-UHFFFAOYSA-L 0.000 description 1
- 235000015320 potassium carbonate Nutrition 0.000 description 1
- 239000012254 powdered material Substances 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 239000005297 pyrex Substances 0.000 description 1
- 150000003248 quinolines Chemical class 0.000 description 1
- 239000012429 reaction media Substances 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 239000012266 salt solution Substances 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 229910000029 sodium carbonate Inorganic materials 0.000 description 1
- 235000017550 sodium carbonate Nutrition 0.000 description 1
- AJPJDKMHJJGVTQ-UHFFFAOYSA-M sodium dihydrogen phosphate Chemical compound [Na+].OP(O)([O-])=O AJPJDKMHJJGVTQ-UHFFFAOYSA-M 0.000 description 1
- 229910001948 sodium oxide Inorganic materials 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- RLQWHDODQVOVKU-UHFFFAOYSA-N tetrapotassium;silicate Chemical compound [K+].[K+].[K+].[K+].[O-][Si]([O-])([O-])[O-] RLQWHDODQVOVKU-UHFFFAOYSA-N 0.000 description 1
- 239000002470 thermal conductor Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
- 239000002341 toxic gas Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003623 transition metal compounds Chemical class 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
- LSGOVYNHVSXFFJ-UHFFFAOYSA-N vanadate(3-) Chemical compound [O-][V]([O-])([O-])=O LSGOVYNHVSXFFJ-UHFFFAOYSA-N 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
- C04B28/24—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing alkyl, ammonium or metal silicates; containing silica sols
- C04B28/26—Silicates of the alkali metals
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C1/00—Ingredients generally applicable to manufacture of glasses, glazes, or vitreous enamels
- C03C1/006—Ingredients generally applicable to manufacture of glasses, glazes, or vitreous enamels to produce glass through wet route
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C25/00—Surface treatment of fibres or filaments made from glass, minerals or slags
- C03C25/10—Coating
- C03C25/42—Coatings containing inorganic materials
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C3/00—Glass compositions
- C03C3/04—Glass compositions containing silica
- C03C3/062—Glass compositions containing silica with less than 40% silica by weight
- C03C3/064—Glass compositions containing silica with less than 40% silica by weight containing boron
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C3/00—Glass compositions
- C03C3/12—Silica-free oxide glass compositions
- C03C3/16—Silica-free oxide glass compositions containing phosphorus
- C03C3/19—Silica-free oxide glass compositions containing phosphorus containing boron
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
- C04B28/006—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing mineral polymers, e.g. geopolymers of the Davidovits type
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements
- C04B28/006—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing mineral polymers, e.g. geopolymers of the Davidovits type
- C04B28/008—Mineral polymers other than those of the Davidovits type, e.g. from a reaction mixture containing waterglass
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00034—Physico-chemical characteristics of the mixtures
- C04B2111/00112—Mixtures characterised by specific pH values
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P40/00—Technologies relating to the processing of minerals
- Y02P40/10—Production of cement, e.g. improving or optimising the production methods; Cement grinding
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Life Sciences & Earth Sciences (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Ceramic Engineering (AREA)
- Geochemistry & Mineralogy (AREA)
- General Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Structural Engineering (AREA)
- Geology (AREA)
- Environmental & Geological Engineering (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Glass Compositions (AREA)
Abstract
A modified alkali silicate composition for forming an inorganic network matrix. The modified alkali silicate matrix is made by reacting an alkali silicate (or its precursors such as an alkali hydroxide, a SiO2 source and water), an acidic inorganic composition, such as a reactive acidic glass, water and optional fillers, additives and processing aids. An inorganic matr ix composite can be prepared by applying a slurry of the modified aqueous alkal i silicate composition to a reinforcing medium and applying the temperature an d pressure necessary to consolidate the desired form. The composite can be shaped by compression molding as well as other known fabrication methods. A notable aspect of the invention is that, although composite and neat resin components prepared from the invention can exhibit excellent dimensional stability to 1000~C and higher, they can be prepared at the lower temperatur es and pressures typical to organic polymer processing.
Description
INORGANIC MATRIX COMPOSITIONS AND
COMPOSITES INCORPORATING THE MATRIX COMPOSITION
s Background of the Invention The present invention relates to inorganic matrix compositions incorporating a silicate network, which can be processed at processing conditions comparable to those used for typical high-performance organic polymer processing (temperatures 15°C to 200°C and pressures <200 psi or 1.378 MPa), although a wide range of temperatures and pressures can be employed. The physical and thermal properties of the inorganic matrix binder as well as composites may be enhanced by elevated processing temperatures (up to 400°C and greater) and pressures (up to 20,000 psi (137.895 MPa) and greater) to produce exceptional composite and neat resin components. The composite materials formed at the lower processing conditions exhibit excellent thermal, dirriensional, physical and flameproof properties: .
Inorganic matrices are useful as flame retardant binders, bulls materials, adhesives or composite materials. As bulk materials, they are used to form shaped objects which when cured provide a structural material. As a composite material, the matrix composition is used to impregnate a fabric, which may be combined with other similarly impregnated fabrics, to form 2o the composite lay-up, which is then shaped and cured to form a shaped object, similar to a bulk material, but with the benefit of the reinforcement provided by the fabric. .
The basic concept of composite materials has been known for centuries.
Composite materials offer a uuque blend of value added features, such as weight savings, electrical insulation, thermal insulation, corrosion resistance, and manufacturing cost savings. These features in some instances can overshadow the material cost in specialized applications ranging, for example, from advanced sporting equipment to the F-22 aircraft fuselage.
However, current state-of the-art composite materials can also exhibit properties that present serious barriers to entry in some high-performance markets. These include poor flame, smoke and toxicity (FST) performance, physical degradation at high temperatures as well as higher material and processing costs. When exposed to fire or high temperatures (>500°C), conventional composite materials can combust and generate toxic smoke and/or gases. The exceptions, such as ceramic matrix composites and metal matrix composites, axe too expensive (often more than $500/lb) to gain a significant market presence. Clearly, a market need exists for affordable high temperature-resistant, insulating structures.
The most familiar composite systems today are based on organic polymer matrices such - as epoxy/glass fiber, epoxy/carbon fiber, polyurethane/glass fiber, PVC/glass fiber, polyimide/quartz fiber, polyester/glass fiber and nylon/glass fiber. Although organic polymer composites exhibit excellent physical and mechanical properties, they are limited with regard to flammability, smoke and gas generation and elevated service temperatures. The flammability of organic polymer-based composites can be reduced by the addition of inorganic components and/or additives. The substitution of hydrogen atoms with halogen atoms (e.g.
chlorine) in hydrocarbons and hydrocarbon polymers can significantly reduce flammability and smoke/gas generation but will degrade at high temperatures (>250°C) and eventually incinerate at higher to temperatures (>450°C). Organic thermoplastic polymers also deform at relatively low temperatures (100°C to 300°C) and organic polymers designed for higher service temperatures are generally prohibitive in material and processing costs.
Other composite materials include metal matrix composites (MMC), ceramic matrix composites (CMC), carbon-carbon composites as well as other inorganic matrix composites. A
composite matrix may be 100% inorganic, or it may contain some organic content. Inorganic matrix networks include ceramics, silicates, glasses, aluminum silicates, alkali aluminum silicates, potassium silicates, sodium silicates, silicon carbides, silicon nitrides, alumina, cementitious materials, metals, metal alloys or other matrix materials known to those knowledgeable in the arts. Other materials can be considered include inorganic particles encapsulated with inorganic binders, organic resins filled with inorganic fillers, inorganic-organic hybrids such as silicone, and other inorganic matrix materials known to those knowledgeable in the arts.
A disadvantage of organic polymers is their deficiencies at high temperatures.
The use of metals and ceramics raises additional questions with regard to thermal and electrical conductivity, weight limitations, toughness, dielectric properties, ductility, and processing options. Further, ceramics do not lend themselves to the low temperature processing procedures as contrasted with organic polymer processing.
A need exists for noncombustible, temperature-resistant inorganic polymer compounds processable at temperatures less than the typical processing temperatures and pressures for organics (<200°C and <200 psi or 1.378 MPa) which combines the desirable features of ceramics (non-flammability, resistance to temperatures >450°C) and organic polymers (low-temperature processing, complex shapes).
COMPOSITES INCORPORATING THE MATRIX COMPOSITION
s Background of the Invention The present invention relates to inorganic matrix compositions incorporating a silicate network, which can be processed at processing conditions comparable to those used for typical high-performance organic polymer processing (temperatures 15°C to 200°C and pressures <200 psi or 1.378 MPa), although a wide range of temperatures and pressures can be employed. The physical and thermal properties of the inorganic matrix binder as well as composites may be enhanced by elevated processing temperatures (up to 400°C and greater) and pressures (up to 20,000 psi (137.895 MPa) and greater) to produce exceptional composite and neat resin components. The composite materials formed at the lower processing conditions exhibit excellent thermal, dirriensional, physical and flameproof properties: .
Inorganic matrices are useful as flame retardant binders, bulls materials, adhesives or composite materials. As bulk materials, they are used to form shaped objects which when cured provide a structural material. As a composite material, the matrix composition is used to impregnate a fabric, which may be combined with other similarly impregnated fabrics, to form 2o the composite lay-up, which is then shaped and cured to form a shaped object, similar to a bulk material, but with the benefit of the reinforcement provided by the fabric. .
The basic concept of composite materials has been known for centuries.
Composite materials offer a uuque blend of value added features, such as weight savings, electrical insulation, thermal insulation, corrosion resistance, and manufacturing cost savings. These features in some instances can overshadow the material cost in specialized applications ranging, for example, from advanced sporting equipment to the F-22 aircraft fuselage.
However, current state-of the-art composite materials can also exhibit properties that present serious barriers to entry in some high-performance markets. These include poor flame, smoke and toxicity (FST) performance, physical degradation at high temperatures as well as higher material and processing costs. When exposed to fire or high temperatures (>500°C), conventional composite materials can combust and generate toxic smoke and/or gases. The exceptions, such as ceramic matrix composites and metal matrix composites, axe too expensive (often more than $500/lb) to gain a significant market presence. Clearly, a market need exists for affordable high temperature-resistant, insulating structures.
The most familiar composite systems today are based on organic polymer matrices such - as epoxy/glass fiber, epoxy/carbon fiber, polyurethane/glass fiber, PVC/glass fiber, polyimide/quartz fiber, polyester/glass fiber and nylon/glass fiber. Although organic polymer composites exhibit excellent physical and mechanical properties, they are limited with regard to flammability, smoke and gas generation and elevated service temperatures. The flammability of organic polymer-based composites can be reduced by the addition of inorganic components and/or additives. The substitution of hydrogen atoms with halogen atoms (e.g.
chlorine) in hydrocarbons and hydrocarbon polymers can significantly reduce flammability and smoke/gas generation but will degrade at high temperatures (>250°C) and eventually incinerate at higher to temperatures (>450°C). Organic thermoplastic polymers also deform at relatively low temperatures (100°C to 300°C) and organic polymers designed for higher service temperatures are generally prohibitive in material and processing costs.
Other composite materials include metal matrix composites (MMC), ceramic matrix composites (CMC), carbon-carbon composites as well as other inorganic matrix composites. A
composite matrix may be 100% inorganic, or it may contain some organic content. Inorganic matrix networks include ceramics, silicates, glasses, aluminum silicates, alkali aluminum silicates, potassium silicates, sodium silicates, silicon carbides, silicon nitrides, alumina, cementitious materials, metals, metal alloys or other matrix materials known to those knowledgeable in the arts. Other materials can be considered include inorganic particles encapsulated with inorganic binders, organic resins filled with inorganic fillers, inorganic-organic hybrids such as silicone, and other inorganic matrix materials known to those knowledgeable in the arts.
A disadvantage of organic polymers is their deficiencies at high temperatures.
The use of metals and ceramics raises additional questions with regard to thermal and electrical conductivity, weight limitations, toughness, dielectric properties, ductility, and processing options. Further, ceramics do not lend themselves to the low temperature processing procedures as contrasted with organic polymer processing.
A need exists for noncombustible, temperature-resistant inorganic polymer compounds processable at temperatures less than the typical processing temperatures and pressures for organics (<200°C and <200 psi or 1.378 MPa) which combines the desirable features of ceramics (non-flammability, resistance to temperatures >450°C) and organic polymers (low-temperature processing, complex shapes).
Alkali silicates are employed as affordable inorganic matrix binder materials.
See for example, US Patent numbers 4,472,199; 4,509,985; 4,888,311; 5,288,321;
5,352,427; 5,539,140;
or 5,798,307 to Davidovits; US Patent number 4,936,939 to Woolum; or US Patent number 4,284,664 to Rauch. However, alkali silicates typically possess a very high pH. Thus, these alkali solutions are so caustic that they damage glass fibers, severely degrading strength.
Furthermore, cured composite samples prepared in accordance to these disclosures still exhibit a high pH in a solid form. Rauch has disclosed the addition of nonreactive borosilicate glass to an alkali silicate solution, but the glass mentioned is Pyrex, a material that is inert.
1 o Summary of the Invention The present invention is the result of the discovery that an inorganic polymer network can be achieved using a composition that is the reaction product of an alkali silicate, a reactive acidic glass and water. The alkali silicate can be prepared either of two ways: (1) As the reaction product of an alkali hydroxide or oxide, a silica source and water or (2) using a commercial or pre-prepared alkali silicate such as Kasil-1, sodium silicate, potassium silicate flake, etc and combinations thereof. Furthermore, inorganic silicate/glass composites can be achieved using an aqueous slurry of a mixture of an alkali silicate (or its precursors), a reactive acidic glass and water, as well as gel inhibitors and other network forming materials and modifiers.
The thermally resistant inorganic matrix compositions of the present invention 2o incorporate a silicate network and an amorphous phosphate glass network that can be processed within a wide range of temperatures and pressures. A useful feature of this invention is the ability to produce high-temperature resin and composite parts capable of withstanding temperatures of 1000°C and are noncombustible. The matrix as well as the composites made from the matrix material exhibit properties generally restricted to ceramics but are cured at temperatures typical for orgaiuc polymer compositions. In addition, the cured matrix composition is not as basic as axe most alkali silicate systems but can be formulated to be near neutral with a typical pH below 8.
The addition of an acidic glass, particularly with favorable physical and mechanical properties can yield an unique cured material for high-temperature applications and components.
The addition of a solid reactive glass powder to the silicate mixture permits a much higher loading of a non-silicate network and lessens the tendency of the mixture to gel prematurely. The combination of two or more networks within the matrix imparts toughness, a near neutral to neutral pH, enhanced temperature resistance (resin and composites >1000°C) and hydrolytic stability.
Alkali silicate/glass-based composites can be prepared by applying an aqueous slurry of the modified alkali silicate/glass matrix precursor to a reinforcing medium such as a continuous or discontinuous glass or carbon fiber mat. After an optional B-staging period the composite is cured using the appropriate temperature and pressure to consolidate the material into a composite. ~ The term "B-staging" is a common term used in composite technology to describe the practice of allowing a polymer matrix precursor to react and proceed to a partially polymerized intermediate stage short of a fully cured polymer network. Vacuum bagging can to also be implemented to aid water removal and consolidation. Compression molding, as well as other typical molding methods, can be used to shape the composite as desired.
The resulting neat resin and/or composite exhibits thermal stability up to 1000°C and higher, depending upon the formulation and processing plus possesses excellent properties with respect to flame, smoke and toxicity. Furthermore, a composite made using the inorganic polymer network forming composition of the present invention is lightweight with good thermal and electrical insulating characteristics. Various shapes are relatively inexpensive to manufacture primarily due to the low temperature and pressures needed to effect cure of the composite.
An alternate composition is a liquid mixture of the alkali base, a silica source, an acidic oxoanionic compound such as phosphoric acid and a multivalent cationic compound such as 2o magnesium nitrate is dried to a friable mass and powdered. The resin powder is combined with the glass powder, formed into usable shape with or without reinforcement, and cured as desired to provide a temperature resistant formulation:
The composition is also useful as an adhesive composition, a coating, a neat resin or as a molding compound. The compositions of the present invention are useful in those applications where good thermal and physical stability are desired, such as those applications for which ceramic composites are used.
Detailed Descr~tion of the Invention The inorganic polymer network of the present invention is prepared by reacting an alkali silicate solution, a reactive acidic glass, water and optionally additives such as a clay and/or an oxide filler. Alternately, the reaction of a silica source, alkali base(s), water and a reactive acidic glass can also yield a high-temperature inorganic polymer network. The composites are made by applying a slurry of an aqueous alkali silicate (or its precursors), a reactive acidic glass (plus any desired additives) and water to a reinforcing medium which can be processed within a wide range of temperatures and pressures. The composite can be shaped by any of the numerous molding methods available prior to curing. The silicate/glass polyner composition can be cured at relatively low temperatures and pressures (i.e., <200°C, and <200 psi or 1.375 MPa) to produce a composite having dimensional and thermal stability to 1000°C
and greater.
The alkali silicates utilized can include a wide range of silicalalkali oxide (Si02/A20) ratios and % solids levels. Such solutions can be purchased from commercial sources or prepared immediately prior to use from precursors such as a silica source and an alkali hydroxide, alkali oxide or carbonate or combination thereof. The alkali silicate can be derived from an alkali base, to such as potassium hydroxide or sodium hydroxide, from potash or soda ash and a silica source.
The Si02 source can be an amorphous or crystalline Si02 form, such as silica, silica fume, precipitated silica, microsilica, sand, microcrystalline silica, silica gels, colloidal silica, quartz, quartz flour, a sodium silicate solution, a potassium silicate solution as well as solid sodium and/or potassium silicates. Various silica sources exhibit desired as well as undesired attributes, for example, some silica fume sources contain traces of carbon that can lead to discoloration in the final product. The thermal and physical properties of the inorganic matrix binder can be influenced by the nature of the silica source, for example, the incorporation of a dense crystalline oc-quartz network can enhance dimensional stability while, in turn, introducing an open, amorphous silica source will produce a lower density network.
When the alkali silicate is derived from an alkali hydroxide and a silica source, the alkali hydroxide is present in an amount of 3 wt. % to 20 wt. % based upon the weight of the total composition or mixture, preferably 7 wt. % to 15 wt. %. The silica source is present in an amount of 10 wt. % to 75 wt. %, preferably 15 wt. % to 60 wt. %. The total mixture, in this instance, includes an alkali hydroxide, a silica source, a reactive acidic glass, water, a clay filler and oxide filler. In some cases, for example, when an alkali silicate solution is used, the portion of the alkali hydroxide, silica and water provided is included in the ranges disclosed.
The phrase "reactive acidic glass" encompasses a wide variety of acidic inorganic glasses that can contribute an acid group in the condensation reaction between the alkali silicate and the glass which occurs during the curing step. Examples of reactive acidic glasses include 3o phosphate, borate and borophosphate glasses. Reactive acidic glasses are different from essentially nonreactive structural glasses as used in beakers and drinking vessels, and optical glasses as used in windows. Reactive acidic glasses are made according to typical glassmaking processes by combining oxide reactants. In the case of an alkali borophosphate glass PZOS, B203, ~5 and one or more alkali oxides or their precursors are combined in a powder form and heating the mixture to its fusion temperature of 700°C to 900°C and then rapidly cooling the melt and optionally annealing the glass to a rigid, friable state. The ratio of phosphoric oxide to alkali metal oxide (A20) will be 6.1:1.0 to 1.5:1Ø The glass solid is then 'pulverized to form a powder.
The reactive acidic glass is preferably in powdered form with reactive borophosphate glass powder being preferred. The thermal and physical properties of the inorganic silicate/glass matrix can be varied by adjusting the ratio of Si02 to the reactive acidic glass (G). The G:Si02 ratio can vary from 0.01 to 50.0 by weight. The reactive acidic glass is used in an amount of to between 0.01% to 60% by weight of the total mixture, with 5% to 35% being preferred, and 10%
to 30% by weight being further preferred.
The glass composition before fusion will comprise 20 mol % to 80 mol % of potassium oxide (PZOS), based upon the total glass formulation, preferably 30 mol % to 70 mol % with 40 mol % to 60 mol % by weight being further preferred. The boron oxide (B2O3) will comprise 1 mol % to 15 mol % of the glass, with 2 mol % to 8 mol % being preferred and 4 mol % to 6 mol further preferred. The alkali oxide (A20) comprises 5 mol % to 50 mol % of the glass composition, with 20 mol % to 40 mol % being preferred, and 15 mol % to 30 mol % further preferred. The alkaline earth oxide (M'O) is used in an amount of between 0.01 mol % to 30 mol of the total glass mixture, with 5 mol % to 20 mol % being preferred, and 10 mol % to 15 mol % being further preferred.
Although the invention is the inorganic matrix composition resulting from the reaction of the alkali silica source and the reactive acidic glass powder, the mechanical, physical and processing characteristics of the matrix can. be enhanced by the addition of reactive and nonreactive fillers such as metal oxides and clays. These optional components if used in the matrix formulation range from 2 wt % to 20 wt %.
The balance of the composition (prior to curing) is water and it will comprise 15% to 60% by weight based upon the total composition weight. The range of 20% to 50%
by weight is preferred, with 25% to 35% by weight further preferred. The water can be contributed as part of one of the components, such as a portion of an alkali silicate solution.
3o An approximate chemical composition of the invention, i.e., a qualitative representation of the starting materials, which is derived from an aqueous mixture before curing to form the inorganic matrix, can be described as follows:
(1-n) [ aA20 : Si02 : gG : fFX] ~ nH20 Where:
A = [(1-z) K20, (z) Na20], where z ranges from 0 to 1.
K20 = potassium oxide to Na20 = sodium oxide Si02 = silica, derived from a silica source such as Kasil-1, silica fume, silica, quartz or silica gel, or a combination thereof.
G = an acidic reactive glass such as an alkaliborophosphate glass.
Fl = (optional) additional network former(s), such as P205, 503, etc., derived from an acidic precursor, such as H3P04, HZS04, etc., or a combination thereof.
F2 = (optional) secondary network linking units) such as Mg2+, Zn2+, Ti4+
derived from 2o multivalent main group metal and/or transition metal compounds such as Mg(N03)Z, Zn(N03)Z, etc. or a combination thereof.
F3 = (optional) reactive and/or rionreactive fillers such as kaolin, mica, vermiculite, metakaolin, metal oxides, etc. or a combination thereof.
F4 = (optional) gelation modifier such as an organic base (quinoline) and/or an organic acid (lactic acid).
H20 = water a = preferred molar ratio of AZO : SiO2 and ranges from 0.05 to 1.00.
g = preferred molar ratio of G : Si02 and ranges is from 0.01 to 50Ø
f = (optional) preferred molar ratio of F : SiOa and ranges from 0.000 to 2.000.
x = 0 to ~20, number of additives (F) used to aid in processing and performance of the basic formulation.
4o n = molar ratio of H20 incorporated into the formulation. During initial formulation, our desired range is from 0.10 to 0.90 (where n = 0.20 to 0.40 is the preferred embodiment). After cure, n is less than 0.25 (where n < 0.05 is the preferred embodiment).
The formulation of the reactive acidic glass (G) is critical to the chemistry and the performance of this invention. It is desired that the glass react with the alkali silicate mixture to reduce the basicity of the resulting matrix and to conjoin multiple networks.
The combination of very different networks, one silicate-based and the other phosphate-based results in a blend of an amorphous inorganic polyner and a crystalline network as well as new network units formed by reaction of the basic silicate and the acidic phosphate such as - Si - O - P -. Both silicate and phosphate species are known to be excellent network formers form the basis for this invention.
The glass (G) can be concisely described by the following formula:
n ~~Mp+~q~~~Eq ~p~~ rkwhere ~Pk = 1 k=1 n = number of desired glass components Where:
M = a main group glass former such as boron, silicon, phosphorus, sulfur, germanium, arsenic, antimony and metallic glass modifiers such as vanadium (also a glass former), titanium, chromiiun, manganese, iron, cobalt, nickel, copper, mercury, zinc, lead, aluminum, zircouum, lanthanum, cerimn, praseodynium, neodymium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, actinium, thorium, uranium, yttrium, gallium, 2o magnesium, calcium, strontium, barium, cadmium, lithium, sodimn, potassium, rubidium, and cesium.
E = oxygen, chalcogenides and halogens such as sulfur (also a glass former), selenium, tellurium and fluorine.
p = cation valence of M such as 5 for phosphorus (generally portrayed as PS+
or P(V)).
q = anion valence of E such as 2 for oxygen (generally portrayed as 02-) q' = number of M cations contained in a network unit equal to q or q/2 whichever is the lesser whole number whenever p and q are even numbers, such as 2 for phosphorus in PZOS or 1 for silicon in Si02.
p' = number of E anions contained in a network unit equal to p or p/2 whichever is the 3o lesser whole number whenever p and q are even numbers, such as 5 for phosphorus in PZOS or 2 for silicon in Si02.
r = molar fraction of each individual network unit in the reactive acidic glass component.
n = number of total network units in the reactive acidic glass component.
Thus for a three-component reactive acidic glass component containing phosphorus, lithium and boron, the generalized formula is:
~~P2~S~r1~L12~~r2~B2~3~r3~
Where: rl + rz + r3 = 1 and rl > r2 For a five-component reactive acidic glass component containing phosphorus, lithium, boron, magnesium and barium, the generalized formula is:
~~~2~5~r1~~'12~)r2~82~3)r3~Mg0)r4~Ba,0)r5~
Wliere: rl + rz + r3 + r4 + r5 = 1 and rl > r2 rl ranges from 0.300 to 0.800, r2 ranges from 0.050 to 0.500, r3 ranges from 0.010 to 0.150, r4 ranges from 0.010 to 0.200, r5 ranges from 0.010 to 0.200.
The chemical and physical properties of the phosphate glass are determined by the initial formulation, the composition of the individual glass components, refining, annealing and aging conditions. The properties of the glass necessary for this invention include an acidic formulation, durability, hydrolytic stability, reactivity and plasticity. The type and ratio of the glass components dictate these properties. For instance, a very reactive yet durable glass can be prepared using NH4HZP04, Li2C03, B(OH)3 and MgC03. The molar ratio of [P205]:[Li20] must be greater than 1 to yield an acidic formulation. The addition of B203 (from B(OH)3) enhances the durability of the phosphate glass while the selection of Li20 (from Li2C03) and Mg0 (from MgC03) reduce water sensitivity. In part, the variation of the molar ratios of all three components govern acidity, durability, hydrolytic stability, the glass softening temperature (TS), the glass melting temperature (Tin) and the glass transition temperature (Tg) of the glass. The refining time and temperature of the glass also influences its physical and mechanical characteristics. For a constant composition increasing the refining temperature andlor time further densifies the glass network raising the Tg, TS and Tm, reducing network activity and the hydroxyl/H20 content of the glass while enhancing durability. Thus by varying the glass composition, the glass refining time and temperature, various glass formulations can differ greatly with regard to reactivity, durability, acidity, hydrolytic stability, toughness and processing. The matching, blending and adjustment of the glass and the alkali silicate properties allows the formulation of a high-temperature material with unique and novel properties. In other words, the ability to vary these "building blocks" enables pne to tailor product properties to suit numerous high-temperature applications.
The matrix composite material system of the present invention addresses the pH
issue by adding an acidic inorganic component (i.e., a reactive acidic glass powder) to an alkali silicate solution. The alkali silicate solutions rely on their high pH to advance the reaction and neutralizing the pH can negatively affect the curing process. The addition of a reactive acidic glass to the alkali silicate component reduces the pH level as the composite is cured, ultimately yielding a near neutral (pH 6-8) cured matrix. This reduces the damage to the glass reinforcement. The cured binder of the present invention contains multiple interacting inorganic to networks, some being amorphous and others being crystalline, based upon the cure conditions.
The combination of multiple networks provides enhanced thermal resistance, controlled chemical reactivity and resistance and reduced water content.
Additional components such as fillers, other network forming materials and modifiers can be incorporated as needed. These include additives and fillers typically used or known to ones skilled in the art. A polymer compound whether inorganic, organic or hybrid can include many additives or fillers to permit processing, fabrication and enhanced performance in service.
Traditional fillers include kaolin, metakaolin, montmorillonites and other clay or mineral fillers.
Modifiers can include crosslinkers and gel inhibitors/promoters such as mineral acids, organic acids and bases. The modified alkali silicate composition that is obtained can be cured at 2o relatively low temperatures (<200°C), and at low pressures (<200 psi or 1.378 MPa) to produce a inorgauc polymer network having dimensional stability to 1000°C and higher. However, it is not restricted to the lower temperature or pressure, and if needed, or desired, properties can be further enhanced utilizing elevated processing temperatures (up to 1000°C and above) and pressures (up to 20,000 psi or 137.895 MPa), or performing post-cure heat treatments.
The optional network former (Fi) compound can be a compound such as borate, sulfate, aluminate, vanadate, boric acid, phosphoric acid, sulfuric acid, nitric acid, sodium dihydrogen phosphate, disodium hydrogen phosphate, potassium hydrogen phosphate, ammonium hydrogen phosphate, germanate, or the like. The optional network former is present in an amount of between 0.0 wt. % and 20 wt. % based upon the total composition. If included in the 3o formulation, the preferred amount of the Fl network former would be between 2 wt. % to 5 wt.
%.
The optional secondary network linking units) (F2) are selected from Groups 2, 3, 4, 5, 11, 12, 13, 14, 15 and 16 of the Periodic Table can be used in an amount of between 0.0 wt.%
to and 10 wt.% based upon the total mixture and if included in the formulation, the range of 1 wt.
to 3 wt. % would be further preferred. The optional secondary network-linking unit can be a multivalent ration useful for coordinating with oxo species such as the alkaline earths, main group metals, transition metal species, lanthanides and/or actinides and any useful combination thereof. Compounds such as Zn(N03)Z can be incorporated to modify network density. Other network linkers can include multivalent rations derived from boron, aluminum, lead, zinc, gallium, cadmium, titanium, zirconium, lanthanum, cerium, neodymium, yttrium, magnesium, calcium, strontium and barium.
The optional clay filler (F3) is preferably calcined kaolin and can be used in an amount from zero to 10 wt. % based upon the weight of the total composition and if included in the formulation, 3 wt. % to 5 wt. % would be further preferred. The calcined kaolin may prove to be reactive with the silicate matrix material, although reactivity of the clay filler is not required and any of the commercially available clay fillers can be employed. ' The optional oxide filler (F3) is preferably magnesium oxide (Mg0) and can be used in an amount of zero % to 10% by weight based upon the total weight of the composition and if included in the formulation 1 % to 6% by weight is preferred and 2% to 4% by weight further preferred.
The optional gel modifier (F4) is an organic acid or base generally selected from the group consisting of hydroxyacids and N-based and P-based bases. Preferably a-hydroxyacids, (3 2o hydroxyacids, substituted pyridines and quinolines are used. These are utilized in an amount from none to 10 wt. % based upon the weight of the total composition, with .OS
wt. % to 5 wt.
being further preferred if used in the formulation.
The balance of the uncured composition is water and it will comprise 10 wt. %
to 75 wt.
based upon the. total composition weight. The range of 15 wt. % to 40 wt. % is further preferred. The water can be introduced as part of one of the components, such as part of an alkali silicate solution, an alkaline earth salt solution or part of a phosphoric acid solution. Since the water incorporated in this invention can be viewed as a reaction medium, a reactant as well as a reaction product, the concentration of water can be difficult to quantify in general. The initial level of water in the starting mixture can vary from 10 wt. % to 70 wt. %
while a B-staged 3o prepreg may contain 5 wt. % to 35 wt. % water. A cured sample of the inorganic binder and/or composite can contain 0 wt. % to 10 wt. % water depending upon the processing conditions.
The reinforcing medium can be a material composed of reinforcing fibers, such as continuous or discontinuous fibers, which will be encapsulated in the matrix material.
Reinforcing fibers may include glass fibers, carbon fibers, graphite fibers, metallic fibers, quartz fibers, ceramic fibers, basalt fibers, silicon carbide fibers, stainless steel fibers, titanium fibers, nickel alloy fibers, polymeric fibers, aramid fibers, alkaline resistant glass fibers and/or other fibers known to those knowledgeable in the arts. Reinforcing fibers may be in many forms, including yarns, tows, whiskers, continuous fibers, short fibers, woven fabrics, knitted fabrics, non-woven fabrics, random mats, felts, braided fabrics, wound tows, and/or other forms known to those knowledgeable in the arts.
The matrix compositions may incorporate a wide variety of organic and inorganic fillers commonly used by those knowledgeable in the art. The matrix may incorporate filler materials l0 such as ceramic powders, mineral powders, silicon carbides, silicon nitrides, carbon, carbon black, molybdenum and its compounds, silicates, aluminmn silicates, sodium aluminum silicates, potassium aluminum silicates or other inorganic fillers known to those knowledgeable in the arts.
Organic materials are less preferred where the application is such that the organic materials will combust and produce gases. The filler materials also could be spheres or particles, such as microspheres, macrospheres, hollow spheres, and solid spheres.
The inorganic matrix of the present invention influences the pH of the solution containing the alkali silicate backbone by incorporating an acidic inorganic component such as a reactive acidic network (e.g. an alkali borophosphate glass). The inorganic matrix binder cures via a condensation reaction partially driven by the elimination of water from the framework and if not removed excessive residual water in the binder leads to poor dimensional stability, poor physical properties and difficulty in processing.
The composite material can be shaped using any of the composite molding methods typically employed. The test specimen for this example was formed into a multi-layer composite by a traditional prepreg/lay-up method. A "prepreg" is formed by impregnating a reinforcing medium or reinforcement with the matrix binder to produce a binder coated fabric sheet. The next step is to layer the individual prepreg plies together to achieve the desired thickness and/or shape. Next, the "lay-up" is placed into a mold to compress and/or consolidate the prepreg and to form the composite shape. Optionally, the prepreg can be subjected to a B-staging period and/or vacuum bagging to reduce the water content. Finally, the composite is cured using the temperature and pressure necessary to consolidate the product.
The uncured composite may come in many forms, such as bulk molding compound, sheet molding compound, powder and reinforcement, liquid and reinforcement and prepreg.
As can be appreciated, the composites of the present invention may be processed by any method capable of applying temperature and/or pressure. Typical processes include compression molding, pultrusion (an automated process capable of producing a constant cross-section product), wet layup (a simple manual process for rapid prototypes and affordable low performance products), filament winding (an automated process for bodies of revolution), autoclave vacuum bag processing (a typical process for high performance aerospace laminates), non-autoclave vacuum bag processing, vacuum infusion (a process for large thick high-performance parts), liquid resin, film infusion or powder infusion, resin transfer molding (a near net-shape molding process with excellent dimensional repeatability), extrusion (a process capable of producing constant cross-section non-structural short-fiber products), injection molding (an automated process capable of producing small non-structural short-fiber products), casting (a process for bulls non-structural products), spin casting (a process capable of producing high-quality tubing), trapped elastomer molding (a process capable of producing unusual shapes) and like processes.
These processes have several advantages compared to the curing/consolidation methods normally used in making high temperature inorganic polymers, namely ceramics and glasses.
Ceramic and glass processing typically requires high temperature processing equipment (above 1000°C). The nature of the inorganic matrix formulation of the present invention allows composites to be processed with conventional equipment found in thousands of composites manufacturing facilities. These processes allow a more rapid throughput than typical ceramic processes and enables the easy manufacturing of larger parts than typical ceramic processes. The use of these 'processes allows high fiber volumes for structural integrity, which is superior to typical concrete processing.
Glass fiber reinforcement (including E-glass fibers, S-glass fibers, alkali resistant glass fibers, etc.) is the preferred reinforcing material and it allows. several unique performance features. The composite materials using glass fiber reinforcement and the matrix binder of the present invention are affordable, non-combustible, thermally-stable (i.e., no substantial or <1.0%
permanent dimensional change after 48 hours of exposure at 700°C) composite materials with insulating qualities and structural qualities that can be processed at lower temperatures using typical processing equipment. Normal processing can be at relatively low temperatures (<200°C) and low pressure (<200 psi or 1.378 MPa). A cross-ply glass fiber laminate can be produced with thermal insulating qualities (e.g., thermal conductivity of nominally 1.4 W/m-K), electrical insulating qualities (no detectable electrical conductivity when measured with a standard ohm meter) and modest mechanical performance (flexural modulus up to 8 Msi, flexural strength up to 20 ksi, and ultimate flexural strains up to 1.3%).
This combination of properties should be enabling technology for many applications.
Ceramic fiber reinforcement (including silicon carbide fibers) is another preferred reinforcement, especially for high temperature applications above 700°C. Although expensive, ceramic fibers maintain structural integrity well above 1000°C. Carbon fiber reinforcement is a .
preferred reinforcement where electrical conductivity, thermal conductivity, high strength and/or impact resistance is desired.
The following material properties and standardized tests are used to evaluate the l0 performance of composites prepared with the inorganic matrix binders of the present invention:
hydrolytic stability; flexural strength (ASTM D790-99), flexural modulus (ASTM
D790-99), ultimate flexural strain (ASTM D790-99), specific gravity (ASTM D792), thermal dimensional stability, thermal conductivity (modified ASTM C177), electrical conductivity;
pH (of the resin solution, the neat resin and the composite structure) Differential Scanning Calorimetry (or DSC);
combustibility, thermal conductivity (ASTM C177), electrical conductivity (ASTM D 257), voltage breakdown (ASTM D229), permittivity @ 1 MHz (ASTM D229), dissipation factor @ 1 MHz (ASTM D229), arc resistance (ASTM D229), Izod impact strength (lengthwise &
crosswise) (ASTM D229), flarmnability (UL 94, ASTM E-1354), dielectric constant;
temperature index (NEMA LI-6), tensile strength, modulus and ultimate strain (ASTM D 638), 2o compression strength, modulus and ultimate strain (ASTM D 695), interlaminar shear strength (ASTM D3846), short beam shear strength (ASTM D2344) and compression after impact.
The formulations disclosed within the terms of the present invention may also comprise any additives and fillers commonly in usage with regular hydraulic binders.
Furthermore, the use of the matrix binder is not solely limited to composites but can be used to form neat resin components, coatings and adhesives.
As can be appreciated, the present invention can be formulated to be non-combustible.
. This desirable safety feature differentiates the invention from most organic materials (such as plastics, wood, rubber, etc.), which tend to combust, generate smoke and/or toxic gases upon exposure to fire. Further, the present invention can be formulated to be a thermal insulator and/or an electrical iizsulator. This desirable feature differentiates compositions in accordance with the present invention from most metals (such as steel, aluminum, copper, etc.), which tend to be thermal conductors and electrical conductors.
The present invention can be formulated to perform at high temperatures (>1000°C) with negligible permanent changes in dimensions. This desirable feature differentiates the invention from most organic materials (which tend to pyrolyze when exposed to temperatures above 500°C), from most cements (which tend to spall above 300°C) and from many metals (including aluminum), which tend to warp or melt at 700°C. As a further feature, the present invention can achieve high temperature performance (above 700°C) while being processed at relatively low temperatures and low pressures (e.g. <200°C and <200 psi or 1.378 MPa).
This feature is desirable because the ability to process at low temperatures and pressures allows the invention to be processed with more affordable equipment and manufacturing processes. This feature of the l0 chemistry differentiates the present invention from most ceramics, glasses and metals, which generally require very lvgh temperatures and/or high pressures to create a molded shape. (Of course, the invention also can be effectively processed at higher temperatures and pressures; we have processed the material above 10,000 psi (68.948 MPa) and above 1500°C).
The present invention can be formulated to impregnate fibers to form a rigid composite material. This desirable feature differentiates the invention from most materials, because most rigid materials have not been processed as a low viscosity liquid capable of wetting fibers. Fiber reinforcements within a matrix material offer many benefits, including improved strength, stiffness, fracture toughness, fatigue strength and impact resistance. While fiber-reinforced composite materials are common in applications ranging from high-performance automotive 2o fascia to F-22 aircraft structures, the vast majority of composite materials are made with organic matrix materials, which are combustible. Non-combustible composite materials, such as ceramic matrix composite materials and metal matrix composite materials, tend to be cost prohibitive (often more than $500 per pound) for most applications. The present invention can be processed at a much lower cost than most ceramic or metal matrix composite materials.
The present invention readily can be formulated to incorporate a wide variety of fillers to tailor the material performance to suit the specific application. These fillers, which may include hollow spheres, conductive fillers, friction additives or thermal additives, can be incorporated to modify physical properties including density, conductivity, coefficient of friction, thermal performance, etc. These desirable features differentiate the present 3o invention from many materials, including many metals. Given these features, the present invention is suited for many applications, including fire barriers, heat shields, high-temperature insulators, high-temperature molds, friction products, tooling and structures in high temperature environments.
The following examples are illustrative of the present invention, and should not limit the scope of the invention.
Glass Preparation:
The following example will serve to illustrate the preparation of a reactive acidic glass for use in accordance with the present invention. The borophosphate glass is prepared as follows (reactants shown in Table 1):
1) The ammonium monobasic phosphate, boric acid, magnesium oxide and lithium 1 o carbonate or their equivalents are combined, blended and ground as dry powders.
If needed, a phosphate/boric acid or other masterbatch can be prepared and used to enhance consistency.
2) The blended mixture is transferred to an alumina crucible and placed in a muffle 15 furnace. The mixture is dried at 150°C for 1-3 hours and then further heated at 225-275°C for 2-10 hours to initiate a low-temperature condensation reaction and minimize foaming at higher temperatures. After the mixture has partially condensed, the furnace temperature is raised to 700-900°C for 0.5 to 5.0 hours.
At completion of the refiung step, the molten glass is poured onto a quench plate 2o and allowed to cool. The glass is then broken into small pieces and ground to the desired particle size, noting that a very small particle size enhances the reactivity of the glass.
3) The glass can be post-treated thermally to limit irregularities in composition, morphology and reactivity.
See for example, US Patent numbers 4,472,199; 4,509,985; 4,888,311; 5,288,321;
5,352,427; 5,539,140;
or 5,798,307 to Davidovits; US Patent number 4,936,939 to Woolum; or US Patent number 4,284,664 to Rauch. However, alkali silicates typically possess a very high pH. Thus, these alkali solutions are so caustic that they damage glass fibers, severely degrading strength.
Furthermore, cured composite samples prepared in accordance to these disclosures still exhibit a high pH in a solid form. Rauch has disclosed the addition of nonreactive borosilicate glass to an alkali silicate solution, but the glass mentioned is Pyrex, a material that is inert.
1 o Summary of the Invention The present invention is the result of the discovery that an inorganic polymer network can be achieved using a composition that is the reaction product of an alkali silicate, a reactive acidic glass and water. The alkali silicate can be prepared either of two ways: (1) As the reaction product of an alkali hydroxide or oxide, a silica source and water or (2) using a commercial or pre-prepared alkali silicate such as Kasil-1, sodium silicate, potassium silicate flake, etc and combinations thereof. Furthermore, inorganic silicate/glass composites can be achieved using an aqueous slurry of a mixture of an alkali silicate (or its precursors), a reactive acidic glass and water, as well as gel inhibitors and other network forming materials and modifiers.
The thermally resistant inorganic matrix compositions of the present invention 2o incorporate a silicate network and an amorphous phosphate glass network that can be processed within a wide range of temperatures and pressures. A useful feature of this invention is the ability to produce high-temperature resin and composite parts capable of withstanding temperatures of 1000°C and are noncombustible. The matrix as well as the composites made from the matrix material exhibit properties generally restricted to ceramics but are cured at temperatures typical for orgaiuc polymer compositions. In addition, the cured matrix composition is not as basic as axe most alkali silicate systems but can be formulated to be near neutral with a typical pH below 8.
The addition of an acidic glass, particularly with favorable physical and mechanical properties can yield an unique cured material for high-temperature applications and components.
The addition of a solid reactive glass powder to the silicate mixture permits a much higher loading of a non-silicate network and lessens the tendency of the mixture to gel prematurely. The combination of two or more networks within the matrix imparts toughness, a near neutral to neutral pH, enhanced temperature resistance (resin and composites >1000°C) and hydrolytic stability.
Alkali silicate/glass-based composites can be prepared by applying an aqueous slurry of the modified alkali silicate/glass matrix precursor to a reinforcing medium such as a continuous or discontinuous glass or carbon fiber mat. After an optional B-staging period the composite is cured using the appropriate temperature and pressure to consolidate the material into a composite. ~ The term "B-staging" is a common term used in composite technology to describe the practice of allowing a polymer matrix precursor to react and proceed to a partially polymerized intermediate stage short of a fully cured polymer network. Vacuum bagging can to also be implemented to aid water removal and consolidation. Compression molding, as well as other typical molding methods, can be used to shape the composite as desired.
The resulting neat resin and/or composite exhibits thermal stability up to 1000°C and higher, depending upon the formulation and processing plus possesses excellent properties with respect to flame, smoke and toxicity. Furthermore, a composite made using the inorganic polymer network forming composition of the present invention is lightweight with good thermal and electrical insulating characteristics. Various shapes are relatively inexpensive to manufacture primarily due to the low temperature and pressures needed to effect cure of the composite.
An alternate composition is a liquid mixture of the alkali base, a silica source, an acidic oxoanionic compound such as phosphoric acid and a multivalent cationic compound such as 2o magnesium nitrate is dried to a friable mass and powdered. The resin powder is combined with the glass powder, formed into usable shape with or without reinforcement, and cured as desired to provide a temperature resistant formulation:
The composition is also useful as an adhesive composition, a coating, a neat resin or as a molding compound. The compositions of the present invention are useful in those applications where good thermal and physical stability are desired, such as those applications for which ceramic composites are used.
Detailed Descr~tion of the Invention The inorganic polymer network of the present invention is prepared by reacting an alkali silicate solution, a reactive acidic glass, water and optionally additives such as a clay and/or an oxide filler. Alternately, the reaction of a silica source, alkali base(s), water and a reactive acidic glass can also yield a high-temperature inorganic polymer network. The composites are made by applying a slurry of an aqueous alkali silicate (or its precursors), a reactive acidic glass (plus any desired additives) and water to a reinforcing medium which can be processed within a wide range of temperatures and pressures. The composite can be shaped by any of the numerous molding methods available prior to curing. The silicate/glass polyner composition can be cured at relatively low temperatures and pressures (i.e., <200°C, and <200 psi or 1.375 MPa) to produce a composite having dimensional and thermal stability to 1000°C
and greater.
The alkali silicates utilized can include a wide range of silicalalkali oxide (Si02/A20) ratios and % solids levels. Such solutions can be purchased from commercial sources or prepared immediately prior to use from precursors such as a silica source and an alkali hydroxide, alkali oxide or carbonate or combination thereof. The alkali silicate can be derived from an alkali base, to such as potassium hydroxide or sodium hydroxide, from potash or soda ash and a silica source.
The Si02 source can be an amorphous or crystalline Si02 form, such as silica, silica fume, precipitated silica, microsilica, sand, microcrystalline silica, silica gels, colloidal silica, quartz, quartz flour, a sodium silicate solution, a potassium silicate solution as well as solid sodium and/or potassium silicates. Various silica sources exhibit desired as well as undesired attributes, for example, some silica fume sources contain traces of carbon that can lead to discoloration in the final product. The thermal and physical properties of the inorganic matrix binder can be influenced by the nature of the silica source, for example, the incorporation of a dense crystalline oc-quartz network can enhance dimensional stability while, in turn, introducing an open, amorphous silica source will produce a lower density network.
When the alkali silicate is derived from an alkali hydroxide and a silica source, the alkali hydroxide is present in an amount of 3 wt. % to 20 wt. % based upon the weight of the total composition or mixture, preferably 7 wt. % to 15 wt. %. The silica source is present in an amount of 10 wt. % to 75 wt. %, preferably 15 wt. % to 60 wt. %. The total mixture, in this instance, includes an alkali hydroxide, a silica source, a reactive acidic glass, water, a clay filler and oxide filler. In some cases, for example, when an alkali silicate solution is used, the portion of the alkali hydroxide, silica and water provided is included in the ranges disclosed.
The phrase "reactive acidic glass" encompasses a wide variety of acidic inorganic glasses that can contribute an acid group in the condensation reaction between the alkali silicate and the glass which occurs during the curing step. Examples of reactive acidic glasses include 3o phosphate, borate and borophosphate glasses. Reactive acidic glasses are different from essentially nonreactive structural glasses as used in beakers and drinking vessels, and optical glasses as used in windows. Reactive acidic glasses are made according to typical glassmaking processes by combining oxide reactants. In the case of an alkali borophosphate glass PZOS, B203, ~5 and one or more alkali oxides or their precursors are combined in a powder form and heating the mixture to its fusion temperature of 700°C to 900°C and then rapidly cooling the melt and optionally annealing the glass to a rigid, friable state. The ratio of phosphoric oxide to alkali metal oxide (A20) will be 6.1:1.0 to 1.5:1Ø The glass solid is then 'pulverized to form a powder.
The reactive acidic glass is preferably in powdered form with reactive borophosphate glass powder being preferred. The thermal and physical properties of the inorganic silicate/glass matrix can be varied by adjusting the ratio of Si02 to the reactive acidic glass (G). The G:Si02 ratio can vary from 0.01 to 50.0 by weight. The reactive acidic glass is used in an amount of to between 0.01% to 60% by weight of the total mixture, with 5% to 35% being preferred, and 10%
to 30% by weight being further preferred.
The glass composition before fusion will comprise 20 mol % to 80 mol % of potassium oxide (PZOS), based upon the total glass formulation, preferably 30 mol % to 70 mol % with 40 mol % to 60 mol % by weight being further preferred. The boron oxide (B2O3) will comprise 1 mol % to 15 mol % of the glass, with 2 mol % to 8 mol % being preferred and 4 mol % to 6 mol further preferred. The alkali oxide (A20) comprises 5 mol % to 50 mol % of the glass composition, with 20 mol % to 40 mol % being preferred, and 15 mol % to 30 mol % further preferred. The alkaline earth oxide (M'O) is used in an amount of between 0.01 mol % to 30 mol of the total glass mixture, with 5 mol % to 20 mol % being preferred, and 10 mol % to 15 mol % being further preferred.
Although the invention is the inorganic matrix composition resulting from the reaction of the alkali silica source and the reactive acidic glass powder, the mechanical, physical and processing characteristics of the matrix can. be enhanced by the addition of reactive and nonreactive fillers such as metal oxides and clays. These optional components if used in the matrix formulation range from 2 wt % to 20 wt %.
The balance of the composition (prior to curing) is water and it will comprise 15% to 60% by weight based upon the total composition weight. The range of 20% to 50%
by weight is preferred, with 25% to 35% by weight further preferred. The water can be contributed as part of one of the components, such as a portion of an alkali silicate solution.
3o An approximate chemical composition of the invention, i.e., a qualitative representation of the starting materials, which is derived from an aqueous mixture before curing to form the inorganic matrix, can be described as follows:
(1-n) [ aA20 : Si02 : gG : fFX] ~ nH20 Where:
A = [(1-z) K20, (z) Na20], where z ranges from 0 to 1.
K20 = potassium oxide to Na20 = sodium oxide Si02 = silica, derived from a silica source such as Kasil-1, silica fume, silica, quartz or silica gel, or a combination thereof.
G = an acidic reactive glass such as an alkaliborophosphate glass.
Fl = (optional) additional network former(s), such as P205, 503, etc., derived from an acidic precursor, such as H3P04, HZS04, etc., or a combination thereof.
F2 = (optional) secondary network linking units) such as Mg2+, Zn2+, Ti4+
derived from 2o multivalent main group metal and/or transition metal compounds such as Mg(N03)Z, Zn(N03)Z, etc. or a combination thereof.
F3 = (optional) reactive and/or rionreactive fillers such as kaolin, mica, vermiculite, metakaolin, metal oxides, etc. or a combination thereof.
F4 = (optional) gelation modifier such as an organic base (quinoline) and/or an organic acid (lactic acid).
H20 = water a = preferred molar ratio of AZO : SiO2 and ranges from 0.05 to 1.00.
g = preferred molar ratio of G : Si02 and ranges is from 0.01 to 50Ø
f = (optional) preferred molar ratio of F : SiOa and ranges from 0.000 to 2.000.
x = 0 to ~20, number of additives (F) used to aid in processing and performance of the basic formulation.
4o n = molar ratio of H20 incorporated into the formulation. During initial formulation, our desired range is from 0.10 to 0.90 (where n = 0.20 to 0.40 is the preferred embodiment). After cure, n is less than 0.25 (where n < 0.05 is the preferred embodiment).
The formulation of the reactive acidic glass (G) is critical to the chemistry and the performance of this invention. It is desired that the glass react with the alkali silicate mixture to reduce the basicity of the resulting matrix and to conjoin multiple networks.
The combination of very different networks, one silicate-based and the other phosphate-based results in a blend of an amorphous inorganic polyner and a crystalline network as well as new network units formed by reaction of the basic silicate and the acidic phosphate such as - Si - O - P -. Both silicate and phosphate species are known to be excellent network formers form the basis for this invention.
The glass (G) can be concisely described by the following formula:
n ~~Mp+~q~~~Eq ~p~~ rkwhere ~Pk = 1 k=1 n = number of desired glass components Where:
M = a main group glass former such as boron, silicon, phosphorus, sulfur, germanium, arsenic, antimony and metallic glass modifiers such as vanadium (also a glass former), titanium, chromiiun, manganese, iron, cobalt, nickel, copper, mercury, zinc, lead, aluminum, zircouum, lanthanum, cerimn, praseodynium, neodymium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, actinium, thorium, uranium, yttrium, gallium, 2o magnesium, calcium, strontium, barium, cadmium, lithium, sodimn, potassium, rubidium, and cesium.
E = oxygen, chalcogenides and halogens such as sulfur (also a glass former), selenium, tellurium and fluorine.
p = cation valence of M such as 5 for phosphorus (generally portrayed as PS+
or P(V)).
q = anion valence of E such as 2 for oxygen (generally portrayed as 02-) q' = number of M cations contained in a network unit equal to q or q/2 whichever is the lesser whole number whenever p and q are even numbers, such as 2 for phosphorus in PZOS or 1 for silicon in Si02.
p' = number of E anions contained in a network unit equal to p or p/2 whichever is the 3o lesser whole number whenever p and q are even numbers, such as 5 for phosphorus in PZOS or 2 for silicon in Si02.
r = molar fraction of each individual network unit in the reactive acidic glass component.
n = number of total network units in the reactive acidic glass component.
Thus for a three-component reactive acidic glass component containing phosphorus, lithium and boron, the generalized formula is:
~~P2~S~r1~L12~~r2~B2~3~r3~
Where: rl + rz + r3 = 1 and rl > r2 For a five-component reactive acidic glass component containing phosphorus, lithium, boron, magnesium and barium, the generalized formula is:
~~~2~5~r1~~'12~)r2~82~3)r3~Mg0)r4~Ba,0)r5~
Wliere: rl + rz + r3 + r4 + r5 = 1 and rl > r2 rl ranges from 0.300 to 0.800, r2 ranges from 0.050 to 0.500, r3 ranges from 0.010 to 0.150, r4 ranges from 0.010 to 0.200, r5 ranges from 0.010 to 0.200.
The chemical and physical properties of the phosphate glass are determined by the initial formulation, the composition of the individual glass components, refining, annealing and aging conditions. The properties of the glass necessary for this invention include an acidic formulation, durability, hydrolytic stability, reactivity and plasticity. The type and ratio of the glass components dictate these properties. For instance, a very reactive yet durable glass can be prepared using NH4HZP04, Li2C03, B(OH)3 and MgC03. The molar ratio of [P205]:[Li20] must be greater than 1 to yield an acidic formulation. The addition of B203 (from B(OH)3) enhances the durability of the phosphate glass while the selection of Li20 (from Li2C03) and Mg0 (from MgC03) reduce water sensitivity. In part, the variation of the molar ratios of all three components govern acidity, durability, hydrolytic stability, the glass softening temperature (TS), the glass melting temperature (Tin) and the glass transition temperature (Tg) of the glass. The refining time and temperature of the glass also influences its physical and mechanical characteristics. For a constant composition increasing the refining temperature andlor time further densifies the glass network raising the Tg, TS and Tm, reducing network activity and the hydroxyl/H20 content of the glass while enhancing durability. Thus by varying the glass composition, the glass refining time and temperature, various glass formulations can differ greatly with regard to reactivity, durability, acidity, hydrolytic stability, toughness and processing. The matching, blending and adjustment of the glass and the alkali silicate properties allows the formulation of a high-temperature material with unique and novel properties. In other words, the ability to vary these "building blocks" enables pne to tailor product properties to suit numerous high-temperature applications.
The matrix composite material system of the present invention addresses the pH
issue by adding an acidic inorganic component (i.e., a reactive acidic glass powder) to an alkali silicate solution. The alkali silicate solutions rely on their high pH to advance the reaction and neutralizing the pH can negatively affect the curing process. The addition of a reactive acidic glass to the alkali silicate component reduces the pH level as the composite is cured, ultimately yielding a near neutral (pH 6-8) cured matrix. This reduces the damage to the glass reinforcement. The cured binder of the present invention contains multiple interacting inorganic to networks, some being amorphous and others being crystalline, based upon the cure conditions.
The combination of multiple networks provides enhanced thermal resistance, controlled chemical reactivity and resistance and reduced water content.
Additional components such as fillers, other network forming materials and modifiers can be incorporated as needed. These include additives and fillers typically used or known to ones skilled in the art. A polymer compound whether inorganic, organic or hybrid can include many additives or fillers to permit processing, fabrication and enhanced performance in service.
Traditional fillers include kaolin, metakaolin, montmorillonites and other clay or mineral fillers.
Modifiers can include crosslinkers and gel inhibitors/promoters such as mineral acids, organic acids and bases. The modified alkali silicate composition that is obtained can be cured at 2o relatively low temperatures (<200°C), and at low pressures (<200 psi or 1.378 MPa) to produce a inorgauc polymer network having dimensional stability to 1000°C and higher. However, it is not restricted to the lower temperature or pressure, and if needed, or desired, properties can be further enhanced utilizing elevated processing temperatures (up to 1000°C and above) and pressures (up to 20,000 psi or 137.895 MPa), or performing post-cure heat treatments.
The optional network former (Fi) compound can be a compound such as borate, sulfate, aluminate, vanadate, boric acid, phosphoric acid, sulfuric acid, nitric acid, sodium dihydrogen phosphate, disodium hydrogen phosphate, potassium hydrogen phosphate, ammonium hydrogen phosphate, germanate, or the like. The optional network former is present in an amount of between 0.0 wt. % and 20 wt. % based upon the total composition. If included in the 3o formulation, the preferred amount of the Fl network former would be between 2 wt. % to 5 wt.
%.
The optional secondary network linking units) (F2) are selected from Groups 2, 3, 4, 5, 11, 12, 13, 14, 15 and 16 of the Periodic Table can be used in an amount of between 0.0 wt.%
to and 10 wt.% based upon the total mixture and if included in the formulation, the range of 1 wt.
to 3 wt. % would be further preferred. The optional secondary network-linking unit can be a multivalent ration useful for coordinating with oxo species such as the alkaline earths, main group metals, transition metal species, lanthanides and/or actinides and any useful combination thereof. Compounds such as Zn(N03)Z can be incorporated to modify network density. Other network linkers can include multivalent rations derived from boron, aluminum, lead, zinc, gallium, cadmium, titanium, zirconium, lanthanum, cerium, neodymium, yttrium, magnesium, calcium, strontium and barium.
The optional clay filler (F3) is preferably calcined kaolin and can be used in an amount from zero to 10 wt. % based upon the weight of the total composition and if included in the formulation, 3 wt. % to 5 wt. % would be further preferred. The calcined kaolin may prove to be reactive with the silicate matrix material, although reactivity of the clay filler is not required and any of the commercially available clay fillers can be employed. ' The optional oxide filler (F3) is preferably magnesium oxide (Mg0) and can be used in an amount of zero % to 10% by weight based upon the total weight of the composition and if included in the formulation 1 % to 6% by weight is preferred and 2% to 4% by weight further preferred.
The optional gel modifier (F4) is an organic acid or base generally selected from the group consisting of hydroxyacids and N-based and P-based bases. Preferably a-hydroxyacids, (3 2o hydroxyacids, substituted pyridines and quinolines are used. These are utilized in an amount from none to 10 wt. % based upon the weight of the total composition, with .OS
wt. % to 5 wt.
being further preferred if used in the formulation.
The balance of the uncured composition is water and it will comprise 10 wt. %
to 75 wt.
based upon the. total composition weight. The range of 15 wt. % to 40 wt. % is further preferred. The water can be introduced as part of one of the components, such as part of an alkali silicate solution, an alkaline earth salt solution or part of a phosphoric acid solution. Since the water incorporated in this invention can be viewed as a reaction medium, a reactant as well as a reaction product, the concentration of water can be difficult to quantify in general. The initial level of water in the starting mixture can vary from 10 wt. % to 70 wt. %
while a B-staged 3o prepreg may contain 5 wt. % to 35 wt. % water. A cured sample of the inorganic binder and/or composite can contain 0 wt. % to 10 wt. % water depending upon the processing conditions.
The reinforcing medium can be a material composed of reinforcing fibers, such as continuous or discontinuous fibers, which will be encapsulated in the matrix material.
Reinforcing fibers may include glass fibers, carbon fibers, graphite fibers, metallic fibers, quartz fibers, ceramic fibers, basalt fibers, silicon carbide fibers, stainless steel fibers, titanium fibers, nickel alloy fibers, polymeric fibers, aramid fibers, alkaline resistant glass fibers and/or other fibers known to those knowledgeable in the arts. Reinforcing fibers may be in many forms, including yarns, tows, whiskers, continuous fibers, short fibers, woven fabrics, knitted fabrics, non-woven fabrics, random mats, felts, braided fabrics, wound tows, and/or other forms known to those knowledgeable in the arts.
The matrix compositions may incorporate a wide variety of organic and inorganic fillers commonly used by those knowledgeable in the art. The matrix may incorporate filler materials l0 such as ceramic powders, mineral powders, silicon carbides, silicon nitrides, carbon, carbon black, molybdenum and its compounds, silicates, aluminmn silicates, sodium aluminum silicates, potassium aluminum silicates or other inorganic fillers known to those knowledgeable in the arts.
Organic materials are less preferred where the application is such that the organic materials will combust and produce gases. The filler materials also could be spheres or particles, such as microspheres, macrospheres, hollow spheres, and solid spheres.
The inorganic matrix of the present invention influences the pH of the solution containing the alkali silicate backbone by incorporating an acidic inorganic component such as a reactive acidic network (e.g. an alkali borophosphate glass). The inorganic matrix binder cures via a condensation reaction partially driven by the elimination of water from the framework and if not removed excessive residual water in the binder leads to poor dimensional stability, poor physical properties and difficulty in processing.
The composite material can be shaped using any of the composite molding methods typically employed. The test specimen for this example was formed into a multi-layer composite by a traditional prepreg/lay-up method. A "prepreg" is formed by impregnating a reinforcing medium or reinforcement with the matrix binder to produce a binder coated fabric sheet. The next step is to layer the individual prepreg plies together to achieve the desired thickness and/or shape. Next, the "lay-up" is placed into a mold to compress and/or consolidate the prepreg and to form the composite shape. Optionally, the prepreg can be subjected to a B-staging period and/or vacuum bagging to reduce the water content. Finally, the composite is cured using the temperature and pressure necessary to consolidate the product.
The uncured composite may come in many forms, such as bulk molding compound, sheet molding compound, powder and reinforcement, liquid and reinforcement and prepreg.
As can be appreciated, the composites of the present invention may be processed by any method capable of applying temperature and/or pressure. Typical processes include compression molding, pultrusion (an automated process capable of producing a constant cross-section product), wet layup (a simple manual process for rapid prototypes and affordable low performance products), filament winding (an automated process for bodies of revolution), autoclave vacuum bag processing (a typical process for high performance aerospace laminates), non-autoclave vacuum bag processing, vacuum infusion (a process for large thick high-performance parts), liquid resin, film infusion or powder infusion, resin transfer molding (a near net-shape molding process with excellent dimensional repeatability), extrusion (a process capable of producing constant cross-section non-structural short-fiber products), injection molding (an automated process capable of producing small non-structural short-fiber products), casting (a process for bulls non-structural products), spin casting (a process capable of producing high-quality tubing), trapped elastomer molding (a process capable of producing unusual shapes) and like processes.
These processes have several advantages compared to the curing/consolidation methods normally used in making high temperature inorganic polymers, namely ceramics and glasses.
Ceramic and glass processing typically requires high temperature processing equipment (above 1000°C). The nature of the inorganic matrix formulation of the present invention allows composites to be processed with conventional equipment found in thousands of composites manufacturing facilities. These processes allow a more rapid throughput than typical ceramic processes and enables the easy manufacturing of larger parts than typical ceramic processes. The use of these 'processes allows high fiber volumes for structural integrity, which is superior to typical concrete processing.
Glass fiber reinforcement (including E-glass fibers, S-glass fibers, alkali resistant glass fibers, etc.) is the preferred reinforcing material and it allows. several unique performance features. The composite materials using glass fiber reinforcement and the matrix binder of the present invention are affordable, non-combustible, thermally-stable (i.e., no substantial or <1.0%
permanent dimensional change after 48 hours of exposure at 700°C) composite materials with insulating qualities and structural qualities that can be processed at lower temperatures using typical processing equipment. Normal processing can be at relatively low temperatures (<200°C) and low pressure (<200 psi or 1.378 MPa). A cross-ply glass fiber laminate can be produced with thermal insulating qualities (e.g., thermal conductivity of nominally 1.4 W/m-K), electrical insulating qualities (no detectable electrical conductivity when measured with a standard ohm meter) and modest mechanical performance (flexural modulus up to 8 Msi, flexural strength up to 20 ksi, and ultimate flexural strains up to 1.3%).
This combination of properties should be enabling technology for many applications.
Ceramic fiber reinforcement (including silicon carbide fibers) is another preferred reinforcement, especially for high temperature applications above 700°C. Although expensive, ceramic fibers maintain structural integrity well above 1000°C. Carbon fiber reinforcement is a .
preferred reinforcement where electrical conductivity, thermal conductivity, high strength and/or impact resistance is desired.
The following material properties and standardized tests are used to evaluate the l0 performance of composites prepared with the inorganic matrix binders of the present invention:
hydrolytic stability; flexural strength (ASTM D790-99), flexural modulus (ASTM
D790-99), ultimate flexural strain (ASTM D790-99), specific gravity (ASTM D792), thermal dimensional stability, thermal conductivity (modified ASTM C177), electrical conductivity;
pH (of the resin solution, the neat resin and the composite structure) Differential Scanning Calorimetry (or DSC);
combustibility, thermal conductivity (ASTM C177), electrical conductivity (ASTM D 257), voltage breakdown (ASTM D229), permittivity @ 1 MHz (ASTM D229), dissipation factor @ 1 MHz (ASTM D229), arc resistance (ASTM D229), Izod impact strength (lengthwise &
crosswise) (ASTM D229), flarmnability (UL 94, ASTM E-1354), dielectric constant;
temperature index (NEMA LI-6), tensile strength, modulus and ultimate strain (ASTM D 638), 2o compression strength, modulus and ultimate strain (ASTM D 695), interlaminar shear strength (ASTM D3846), short beam shear strength (ASTM D2344) and compression after impact.
The formulations disclosed within the terms of the present invention may also comprise any additives and fillers commonly in usage with regular hydraulic binders.
Furthermore, the use of the matrix binder is not solely limited to composites but can be used to form neat resin components, coatings and adhesives.
As can be appreciated, the present invention can be formulated to be non-combustible.
. This desirable safety feature differentiates the invention from most organic materials (such as plastics, wood, rubber, etc.), which tend to combust, generate smoke and/or toxic gases upon exposure to fire. Further, the present invention can be formulated to be a thermal insulator and/or an electrical iizsulator. This desirable feature differentiates compositions in accordance with the present invention from most metals (such as steel, aluminum, copper, etc.), which tend to be thermal conductors and electrical conductors.
The present invention can be formulated to perform at high temperatures (>1000°C) with negligible permanent changes in dimensions. This desirable feature differentiates the invention from most organic materials (which tend to pyrolyze when exposed to temperatures above 500°C), from most cements (which tend to spall above 300°C) and from many metals (including aluminum), which tend to warp or melt at 700°C. As a further feature, the present invention can achieve high temperature performance (above 700°C) while being processed at relatively low temperatures and low pressures (e.g. <200°C and <200 psi or 1.378 MPa).
This feature is desirable because the ability to process at low temperatures and pressures allows the invention to be processed with more affordable equipment and manufacturing processes. This feature of the l0 chemistry differentiates the present invention from most ceramics, glasses and metals, which generally require very lvgh temperatures and/or high pressures to create a molded shape. (Of course, the invention also can be effectively processed at higher temperatures and pressures; we have processed the material above 10,000 psi (68.948 MPa) and above 1500°C).
The present invention can be formulated to impregnate fibers to form a rigid composite material. This desirable feature differentiates the invention from most materials, because most rigid materials have not been processed as a low viscosity liquid capable of wetting fibers. Fiber reinforcements within a matrix material offer many benefits, including improved strength, stiffness, fracture toughness, fatigue strength and impact resistance. While fiber-reinforced composite materials are common in applications ranging from high-performance automotive 2o fascia to F-22 aircraft structures, the vast majority of composite materials are made with organic matrix materials, which are combustible. Non-combustible composite materials, such as ceramic matrix composite materials and metal matrix composite materials, tend to be cost prohibitive (often more than $500 per pound) for most applications. The present invention can be processed at a much lower cost than most ceramic or metal matrix composite materials.
The present invention readily can be formulated to incorporate a wide variety of fillers to tailor the material performance to suit the specific application. These fillers, which may include hollow spheres, conductive fillers, friction additives or thermal additives, can be incorporated to modify physical properties including density, conductivity, coefficient of friction, thermal performance, etc. These desirable features differentiate the present 3o invention from many materials, including many metals. Given these features, the present invention is suited for many applications, including fire barriers, heat shields, high-temperature insulators, high-temperature molds, friction products, tooling and structures in high temperature environments.
The following examples are illustrative of the present invention, and should not limit the scope of the invention.
Glass Preparation:
The following example will serve to illustrate the preparation of a reactive acidic glass for use in accordance with the present invention. The borophosphate glass is prepared as follows (reactants shown in Table 1):
1) The ammonium monobasic phosphate, boric acid, magnesium oxide and lithium 1 o carbonate or their equivalents are combined, blended and ground as dry powders.
If needed, a phosphate/boric acid or other masterbatch can be prepared and used to enhance consistency.
2) The blended mixture is transferred to an alumina crucible and placed in a muffle 15 furnace. The mixture is dried at 150°C for 1-3 hours and then further heated at 225-275°C for 2-10 hours to initiate a low-temperature condensation reaction and minimize foaming at higher temperatures. After the mixture has partially condensed, the furnace temperature is raised to 700-900°C for 0.5 to 5.0 hours.
At completion of the refiung step, the molten glass is poured onto a quench plate 2o and allowed to cool. The glass is then broken into small pieces and ground to the desired particle size, noting that a very small particle size enhances the reactivity of the glass.
3) The glass can be post-treated thermally to limit irregularities in composition, morphology and reactivity.
Table 1: The initial formulations of the phosphate glasses described in Examples 1-5.
Ingredient Example Example Example Example Example NH~HZPOd 90.40 132.86 148.94 126.53 88.83 B(OH)3 3.21 6.44 6.36 6.43 3.16 MgC03 1.58 8.85 8.73 8.83 3.25 BaC03 ~ - 20.72 5.11 20.67 -Li2(C03)2 4.84 15.52 15.31 17.42 4.17 Refining 250C / 500C / 4 500C / 500C / 4 110C l 3 4 hrs. hrs. 2 hrs. hrs. hrs.
Conditions 750C / 900C / 4 900C / 900C / 4 230C / 18 5 hrs. hrs. 4 hrs. hrs. hrs.
T(C) / t(min) 715C / 1 hrs.
The examples illustrate the preparation of the reactive acidic glasses which will be used in examples 6 - 11, which follow. The glass is prepared by blending the ingredients shown in Table 1. The blended mixture is put into alumina crucibles and placed in a muffle furnace at the conditions given in the table. The molten glass in poured onto a quench plate and allowed to cool. The glass is then ground to the desired particle size.
to Example 6 A portion of I~asil-1 (9.0 g) is transferred to a SOmL beaker and slightly diluted by adding a small amount of water (1.0 g). The beaker is stirred and allowed to cool to ambient temperature. Next the phosphate glass prepared according to Example 1 is added slowly to the stirred potassium silicate solution. After this addition is completed, calcined kaolin, metakaolin or kaolin powder (1.0 g) is added with high-shear mixing. The mixture is allowed to set until the viscosity comes to a level (approximately 150 centipoise) suitable for application to the reinforcement medium (fabric, chopped fiber, wound filament, etc.) needed to construct the composite. If a neat sample is required, the amount of water used can be reduced. The composite material can be prepared using any of the composite molding methods typically 2o employed, the test specimen for this example was formed into a composite by a traditional prepreg/lay-up method. A "prepreg" is formed by impregnating a reinforcing medium or reinforcement with the matrix binder to produce a binder coated fabric sheet.
The next step is to layer the individual prepregs together to achieve the desired tluckness and/or shape. Next, the "lay-up" is placed into a mold to compact or consolidate the prepregs amd to form the composite shape. Optionally, the prepregs could be subjected to a B-staging period and/or vacuum bagging to reduce the water content.
Fiberglass composite panels were made using this formulation and compression molded using standard composite processing parameters: curing at 200 psi (or 1.378 MPa) and 80°C for 3 hours, 110°C for 3 hours and 150°C for 3 hours.
Exam lp a 7:
Potassium hydroxide (52.2 gms) is dissolved in water (148.2 gms) by stirnng.
This dissolution is exothermic requiring cooling (refrigerating to approximately 5°C) before adding l0 the remaiung ingredients. The silica fume (301.2 gms) is then added to the chilled solution slowly using high shear, continually monitoring the temperature. This mixture is allowed to stir for approximately 5 minutes before adding lactic acid (9 gms) after which it is allowed to stir for an additional 5 minutes. The glass (75 gms), made in example 2, is suspended in water (20.1 gms) and slowly added using high shear to the mixture. Finally, kaolin (28.2 gms) then magnesium oxide (28.2 gms) are added using high sheax mixing. The mixture is stirred for an additional 10 minutes resulting in a material with a viscosity of approximately 20,000 cp.
Prepreg is made from combining this material with a reinforcing fabric.
Impregnation and curing process is described in Example 12.
Example 8:
Potassium hydroxide (43.5 gms) is dissolved in water (123.5 gms) by stirring.
This dissolution is exothermic requiring cooling (refrigerating to approximately 5°C) before adding the remaining ingredients. Tamsil 8 (200.8 gms) and silica gel (50.2gms) are then added to the chilled solution slowly using high shear, continually monitoring the temperature. The glass (125 gms) made in example 3 is suspended in water (33.5 gms) and added slowly to the mixture using high shear mixing. Finally, kaolin (23.5 gms) then magnesium oxide (23.5 gms) are added using high shear mixing. The mixture is stirred for an additional 10 minutes resulting in a material with a viscosity of approximately 100,000 cp. Prepreg is made from combining this material with a reinforcing fabric. Impregnation and curing process is described in Example 13.
Example 9:
Silica fume (5.2 gms) is added to Kasil 1 (130.0 gms) and stirred for 10 minutes. The-glass (80.0 gms) made in example 4 is suspended in water (30.0 gms) and added to the mixture slowly using a high shear mixer. Kaolin (7.5 gms) and magnesium oxide (7.5 gms) are then slowly added separately using lugh shear mixing. The mixture is then stirred for an additional 10 minutes resulting in a low viscosity (approximately 150 cp) mixture. Prepreg is made from combining this material with a reinforcing fabric. Impregnation and curing process is described in Example 14.
Example 10:
Potassium hydroxide (10.0 gms) is dissolved in water (70.0 gms) by stirring.
The silica fume (30.0 gms) is then added to the solution slowly with high shear mixing.
The glass (80.0 gms) made in example 5 is suspended in water (30.0 gms) and added slowly to the mixture with to vigorous stirring. Finally, kaolin (7.5 gms) then magnesium oxide (7.5) are added using high shear mixing. The mixture is stirred for an additional 30 minutes resulting in a material with a viscosity of approximately 100 cp. Prepreg is made from combining this material with a reinforcing fabric. Impregnation and curing process is described in Example 15.
Example 11:
Potassium hydroxide (10.0 gms) is dissolved in water (100.0 gms) with stirring and allowed to cool. The silica fume (30.0 gms) is then added to the solution slowly with high shear stirring. After mixing for approximately 20 minutes the mixture is poured into' flat dish, creating a liquid layer approximately 0.25" thick, and allowed to dry for 3 days. The dry material is then 2o milled to fine powder. A second powder is made by blending the glass powder (80.0 gms) made in Example 5 with kaolin (7.5 gms) and magnesium oxide (7.5 gms). The two powders are then blended together to be used in molding and/or prepreg techniques. Impregnation and curing process is described.in Example 16.
Example 12:
The resin formulation made in Example 7 is poured into a lab prepreg apparatus consisting of a resin bath and squeeze roll. The glass fabric, S2-Glass 6781, is fed through the bath and squeeze rolls impregnating the fabric with the resin formulation. The prepreg is then allowed to stage at room temperature for 30 minutes at which time the resin will not transfer when touched. The staged prepreg is cut into plies and layered on a metal plate. The lay-up is then vacuum bagged and a vacuum of 28 inches is pulled on the part for 2 hours. After 2 hours at room temperature the part is put into the press at 80°C and 200 psi (or 1.378 MPa) for 3 hrs completing the cure cycle (refer to Table 2 for flexural properties).
Exam 1pe13:
The resin formulation made in Example 8 is impregnated into the glass fabric, S2-Glass 6781, manually using a plastic spool. The prepreg is staged at room temperature for 30 minutes at which time the resin is slightly sticky. The staged prepreg is cut into plies and layered on a metal plate. The lay-up is then vacuum bagged and a vacuum of 28 inches (0.98138 Kgf/cm2) is pulled on the part for 2 hours. After 2 hours at room temperature the part is put into the press at 80°C and 200 psi (or 1.378 MPa) for 4 hrs., 110°C and 200 psi (or 1.378 MPa) for 2 hrs. and 150°C and 200 psi (or 1.378 MPa) for 2 hrs. (refer to Table 2 for flexural properties).
Example 14:
The resin formulation made in Example 9 is poured into a lab prepreg apparatus consisting of a resin bath and squeeze rolls. The glass fabric, E-Glass 7781, is fed through the bath and squeeze rolls impregnating the fabric with the resin formulation. The prepreg is then allowed to stage at room temperature overnight at which time the resin becomes dry to the touch.
The staged prepreg is cut into plies and inserted into a mold. The mold is then put into the press and cure at 85°C and 200 psi (or 1.378 MPa) for 2 hrs., 110°C
and 200 psi (or 1.378 MPa) for 1 hr., and 175°C and 200 psi (or 1.378 MPa) for 2 hrs. (refer to Table 2 for flexural properties).
Example 15:
The resin formulation made in Example 10 is poured into a lab prepreg apparatus consisting of a resin bath and squeeze rolls. The glass fabric, E-Glass 7781, is fed through the bath and squeeze rolls impregnating.the fabric with the resin formulation. The prepreg is then allowed to stage at room temperature overnight at which time the resin becomes dry to the touch.
The staged prepreg is cut into plies and inserted into a mold. The mold is then put into the press and cured at 120°C and 200 psi (1.378 MPa) for 1 hr. and 175 °C
and 200 psi (1.378 MPa) for 4 hrs. (refer to Table 2 for flexural properties).
Example 16:
The powdered material made in Example 11 is spread into a thin layer over a single ply of glass, the weight of the glass ply and powder are approximately equal. This same process is repeated for multiple plies then stacked into a laminate consisting of glass ply / powder / glass ply / powder. The laminate is inserted into a mold and press cured at 120°C and 200 psi (I.378 MPa) for 1 hr. and 175°C and 200 psi (1.378 MPa) for 4 hrs. (refer to Table 2 for flexural properties).
Table 2: Flexural Properties of samples tested in Examples 12 -16.
Example Flexural StrengthFlexural Modulus (Msi) Ultimate (I~si) Strain 12 14.75 (101.698 3.347 (23,076.8 MPa) 0.00564 MPa) 13 11.40 (78.600 4.295 (29,613.0 MPa) 0.00329 MPa) 14 11.52 (79.428 2.221 (15,313.3 MPa) 0.00280 MPa) 15 ~ 10.42 (71.843 3.300 (22,752.7 MPa) -MPa) 16 10.97 (75.635 2.745 (18,926.1 MPa) -MPa) Composites made in accordance with the present invention may be used in a wide variety of applications such as reinforced missile silo doors, ship decks, blast shields for aircraft carrier decks, hot gas filters, protective coatings, electrical panels and boxes (with and without EMI
shielding), engine covers and heat shields where it would provide, advantageously, corrosion l0 resistance, lifecycle cost savings and weight reduction. Another example would be reinforced insulator inserts for aircraft brakes. The insulator within each piston thermally isolates ~ the friction head from the hydraulic system. Compared to conventional resins, which decompose below 450°C, the matrix binders of the present invention have much higher thermal stability (to above 800°C), and in contrast to metals, the composite of the present invention has superior insulation performance. This protects the hydraulic system and can reduce the weight and/or associated costs. In comparison to ceramics, the composite of the present invention is tougher because due to the presence of the reinforcing fibers, but less expensive than ceramic matrix composites due to the materials and processes utilized.
The foregoing embodiments of the present invention have been presented for the 2o purposes of illustration and description. These descriptions and embodiments are not intended to be exhaustive or to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above disclosure.
The embodiments were chosen and described in order to best explain the principle of the invention and its practical applications to thereby enable others skilled in the art to best utilize the invention in its various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the invention be defined by the following claims.
Ingredient Example Example Example Example Example NH~HZPOd 90.40 132.86 148.94 126.53 88.83 B(OH)3 3.21 6.44 6.36 6.43 3.16 MgC03 1.58 8.85 8.73 8.83 3.25 BaC03 ~ - 20.72 5.11 20.67 -Li2(C03)2 4.84 15.52 15.31 17.42 4.17 Refining 250C / 500C / 4 500C / 500C / 4 110C l 3 4 hrs. hrs. 2 hrs. hrs. hrs.
Conditions 750C / 900C / 4 900C / 900C / 4 230C / 18 5 hrs. hrs. 4 hrs. hrs. hrs.
T(C) / t(min) 715C / 1 hrs.
The examples illustrate the preparation of the reactive acidic glasses which will be used in examples 6 - 11, which follow. The glass is prepared by blending the ingredients shown in Table 1. The blended mixture is put into alumina crucibles and placed in a muffle furnace at the conditions given in the table. The molten glass in poured onto a quench plate and allowed to cool. The glass is then ground to the desired particle size.
to Example 6 A portion of I~asil-1 (9.0 g) is transferred to a SOmL beaker and slightly diluted by adding a small amount of water (1.0 g). The beaker is stirred and allowed to cool to ambient temperature. Next the phosphate glass prepared according to Example 1 is added slowly to the stirred potassium silicate solution. After this addition is completed, calcined kaolin, metakaolin or kaolin powder (1.0 g) is added with high-shear mixing. The mixture is allowed to set until the viscosity comes to a level (approximately 150 centipoise) suitable for application to the reinforcement medium (fabric, chopped fiber, wound filament, etc.) needed to construct the composite. If a neat sample is required, the amount of water used can be reduced. The composite material can be prepared using any of the composite molding methods typically 2o employed, the test specimen for this example was formed into a composite by a traditional prepreg/lay-up method. A "prepreg" is formed by impregnating a reinforcing medium or reinforcement with the matrix binder to produce a binder coated fabric sheet.
The next step is to layer the individual prepregs together to achieve the desired tluckness and/or shape. Next, the "lay-up" is placed into a mold to compact or consolidate the prepregs amd to form the composite shape. Optionally, the prepregs could be subjected to a B-staging period and/or vacuum bagging to reduce the water content.
Fiberglass composite panels were made using this formulation and compression molded using standard composite processing parameters: curing at 200 psi (or 1.378 MPa) and 80°C for 3 hours, 110°C for 3 hours and 150°C for 3 hours.
Exam lp a 7:
Potassium hydroxide (52.2 gms) is dissolved in water (148.2 gms) by stirnng.
This dissolution is exothermic requiring cooling (refrigerating to approximately 5°C) before adding l0 the remaiung ingredients. The silica fume (301.2 gms) is then added to the chilled solution slowly using high shear, continually monitoring the temperature. This mixture is allowed to stir for approximately 5 minutes before adding lactic acid (9 gms) after which it is allowed to stir for an additional 5 minutes. The glass (75 gms), made in example 2, is suspended in water (20.1 gms) and slowly added using high shear to the mixture. Finally, kaolin (28.2 gms) then magnesium oxide (28.2 gms) are added using high sheax mixing. The mixture is stirred for an additional 10 minutes resulting in a material with a viscosity of approximately 20,000 cp.
Prepreg is made from combining this material with a reinforcing fabric.
Impregnation and curing process is described in Example 12.
Example 8:
Potassium hydroxide (43.5 gms) is dissolved in water (123.5 gms) by stirring.
This dissolution is exothermic requiring cooling (refrigerating to approximately 5°C) before adding the remaining ingredients. Tamsil 8 (200.8 gms) and silica gel (50.2gms) are then added to the chilled solution slowly using high shear, continually monitoring the temperature. The glass (125 gms) made in example 3 is suspended in water (33.5 gms) and added slowly to the mixture using high shear mixing. Finally, kaolin (23.5 gms) then magnesium oxide (23.5 gms) are added using high shear mixing. The mixture is stirred for an additional 10 minutes resulting in a material with a viscosity of approximately 100,000 cp. Prepreg is made from combining this material with a reinforcing fabric. Impregnation and curing process is described in Example 13.
Example 9:
Silica fume (5.2 gms) is added to Kasil 1 (130.0 gms) and stirred for 10 minutes. The-glass (80.0 gms) made in example 4 is suspended in water (30.0 gms) and added to the mixture slowly using a high shear mixer. Kaolin (7.5 gms) and magnesium oxide (7.5 gms) are then slowly added separately using lugh shear mixing. The mixture is then stirred for an additional 10 minutes resulting in a low viscosity (approximately 150 cp) mixture. Prepreg is made from combining this material with a reinforcing fabric. Impregnation and curing process is described in Example 14.
Example 10:
Potassium hydroxide (10.0 gms) is dissolved in water (70.0 gms) by stirring.
The silica fume (30.0 gms) is then added to the solution slowly with high shear mixing.
The glass (80.0 gms) made in example 5 is suspended in water (30.0 gms) and added slowly to the mixture with to vigorous stirring. Finally, kaolin (7.5 gms) then magnesium oxide (7.5) are added using high shear mixing. The mixture is stirred for an additional 30 minutes resulting in a material with a viscosity of approximately 100 cp. Prepreg is made from combining this material with a reinforcing fabric. Impregnation and curing process is described in Example 15.
Example 11:
Potassium hydroxide (10.0 gms) is dissolved in water (100.0 gms) with stirring and allowed to cool. The silica fume (30.0 gms) is then added to the solution slowly with high shear stirring. After mixing for approximately 20 minutes the mixture is poured into' flat dish, creating a liquid layer approximately 0.25" thick, and allowed to dry for 3 days. The dry material is then 2o milled to fine powder. A second powder is made by blending the glass powder (80.0 gms) made in Example 5 with kaolin (7.5 gms) and magnesium oxide (7.5 gms). The two powders are then blended together to be used in molding and/or prepreg techniques. Impregnation and curing process is described.in Example 16.
Example 12:
The resin formulation made in Example 7 is poured into a lab prepreg apparatus consisting of a resin bath and squeeze roll. The glass fabric, S2-Glass 6781, is fed through the bath and squeeze rolls impregnating the fabric with the resin formulation. The prepreg is then allowed to stage at room temperature for 30 minutes at which time the resin will not transfer when touched. The staged prepreg is cut into plies and layered on a metal plate. The lay-up is then vacuum bagged and a vacuum of 28 inches is pulled on the part for 2 hours. After 2 hours at room temperature the part is put into the press at 80°C and 200 psi (or 1.378 MPa) for 3 hrs completing the cure cycle (refer to Table 2 for flexural properties).
Exam 1pe13:
The resin formulation made in Example 8 is impregnated into the glass fabric, S2-Glass 6781, manually using a plastic spool. The prepreg is staged at room temperature for 30 minutes at which time the resin is slightly sticky. The staged prepreg is cut into plies and layered on a metal plate. The lay-up is then vacuum bagged and a vacuum of 28 inches (0.98138 Kgf/cm2) is pulled on the part for 2 hours. After 2 hours at room temperature the part is put into the press at 80°C and 200 psi (or 1.378 MPa) for 4 hrs., 110°C and 200 psi (or 1.378 MPa) for 2 hrs. and 150°C and 200 psi (or 1.378 MPa) for 2 hrs. (refer to Table 2 for flexural properties).
Example 14:
The resin formulation made in Example 9 is poured into a lab prepreg apparatus consisting of a resin bath and squeeze rolls. The glass fabric, E-Glass 7781, is fed through the bath and squeeze rolls impregnating the fabric with the resin formulation. The prepreg is then allowed to stage at room temperature overnight at which time the resin becomes dry to the touch.
The staged prepreg is cut into plies and inserted into a mold. The mold is then put into the press and cure at 85°C and 200 psi (or 1.378 MPa) for 2 hrs., 110°C
and 200 psi (or 1.378 MPa) for 1 hr., and 175°C and 200 psi (or 1.378 MPa) for 2 hrs. (refer to Table 2 for flexural properties).
Example 15:
The resin formulation made in Example 10 is poured into a lab prepreg apparatus consisting of a resin bath and squeeze rolls. The glass fabric, E-Glass 7781, is fed through the bath and squeeze rolls impregnating.the fabric with the resin formulation. The prepreg is then allowed to stage at room temperature overnight at which time the resin becomes dry to the touch.
The staged prepreg is cut into plies and inserted into a mold. The mold is then put into the press and cured at 120°C and 200 psi (1.378 MPa) for 1 hr. and 175 °C
and 200 psi (1.378 MPa) for 4 hrs. (refer to Table 2 for flexural properties).
Example 16:
The powdered material made in Example 11 is spread into a thin layer over a single ply of glass, the weight of the glass ply and powder are approximately equal. This same process is repeated for multiple plies then stacked into a laminate consisting of glass ply / powder / glass ply / powder. The laminate is inserted into a mold and press cured at 120°C and 200 psi (I.378 MPa) for 1 hr. and 175°C and 200 psi (1.378 MPa) for 4 hrs. (refer to Table 2 for flexural properties).
Table 2: Flexural Properties of samples tested in Examples 12 -16.
Example Flexural StrengthFlexural Modulus (Msi) Ultimate (I~si) Strain 12 14.75 (101.698 3.347 (23,076.8 MPa) 0.00564 MPa) 13 11.40 (78.600 4.295 (29,613.0 MPa) 0.00329 MPa) 14 11.52 (79.428 2.221 (15,313.3 MPa) 0.00280 MPa) 15 ~ 10.42 (71.843 3.300 (22,752.7 MPa) -MPa) 16 10.97 (75.635 2.745 (18,926.1 MPa) -MPa) Composites made in accordance with the present invention may be used in a wide variety of applications such as reinforced missile silo doors, ship decks, blast shields for aircraft carrier decks, hot gas filters, protective coatings, electrical panels and boxes (with and without EMI
shielding), engine covers and heat shields where it would provide, advantageously, corrosion l0 resistance, lifecycle cost savings and weight reduction. Another example would be reinforced insulator inserts for aircraft brakes. The insulator within each piston thermally isolates ~ the friction head from the hydraulic system. Compared to conventional resins, which decompose below 450°C, the matrix binders of the present invention have much higher thermal stability (to above 800°C), and in contrast to metals, the composite of the present invention has superior insulation performance. This protects the hydraulic system and can reduce the weight and/or associated costs. In comparison to ceramics, the composite of the present invention is tougher because due to the presence of the reinforcing fibers, but less expensive than ceramic matrix composites due to the materials and processes utilized.
The foregoing embodiments of the present invention have been presented for the 2o purposes of illustration and description. These descriptions and embodiments are not intended to be exhaustive or to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above disclosure.
The embodiments were chosen and described in order to best explain the principle of the invention and its practical applications to thereby enable others skilled in the art to best utilize the invention in its various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the invention be defined by the following claims.
Claims (54)
1. An inorganic matrix composition comprising the reaction product of an alkali silicate and/or alkali silicate precursors, a reactive acidic glass, water, and optionally a clay and/or oxide filler.
2. The composition of claim 1, wherein the alkali silicate is selected from potassium silicate solutions and/or sodium silicate solutions.
3. The composition, of claim 1, wherein the alkali silicate is crystalline and/or amorphous sodium silicate and/or potassium silicate.
4. The composition of claim 1 wherein the alkali silicate precursors are alkali hydroxides and a SiO2 source.
5. The composition of claim 4 wherein the SiO2 source is an amorphous or crystalline SiO2 form, selected from the group consisting of silica, silica fume, microsilica, precipitated silica, sand, quartz, quartz flour, silica gels, fumed silica and colloidal silica.
6. The composition of claim 4 wherein the alkali hydroxide is selected from the group consisting of potassium hydroxide and sodium hydroxide.
7. The composition of claim 1 wherein the alkali silicate and/or alkali silicate precursors has a SiO2/A2O ratio of 2.0:1.0 to 20.0:1.0, where A is K (potassium) and/or Na (sodium).
8. The composition of claim 1, wherein said acidic reactive glass is selected from the group of consisting of phosphate glasses, borate glasses and sulfate glasses.
9. The composition of claim 1, wherein the acidic reactive glass is selected from the group of consisting of phosphate glasses such as ultraphosphate glasses, borophosphate glasses, alkaliborophosphate glasses, silicophosphate glasses, aluminophosphate glasses and mixtures thereof.
10. The composition of claim 1, wherein the acidic reactive glass is selected from the group of consisting of phosphate glasses such as ultraphosphate glasses, borophosphate glasses, silicophosphate glasses, aluminophosphate glasses and mixtures thereof.
11. The composition of claim 1, wherein the acidic reactive glass is an alkali borophosphate glass.
12. The composition of claim 1, wherein the acidic reactive glass is an acidic alkali borophosphate glass.
13. The composition of claim 1, wherein the glass comprises the following formula:
[(M p+)q')(E q-)p+]r where M is a main group glass former and/or a metallic glass modifier, E is an oxygen, chalcogenide and/or a halogen atom, p is the cation valence of M, q is the anion valence of E, q' is number of M cations contained in a network unit, p' is number of E anions contained in a network unit and r is the molar fraction of that network unit.
[(M p+)q')(E q-)p+]r where M is a main group glass former and/or a metallic glass modifier, E is an oxygen, chalcogenide and/or a halogen atom, p is the cation valence of M, q is the anion valence of E, q' is number of M cations contained in a network unit, p' is number of E anions contained in a network unit and r is the molar fraction of that network unit.
14. The composition of claim 13 wherein M is a main group glass former selected from the group consisting of boron, silicon, phosphorus, sulfur, germanium, arsenic, antimony and metallic glass modifiers such as vanadium (also a glass former), titanium, chromium, manganese, iron, cobalt, nickel, copper, mercury, zinc, tin, lead, aluminum, zirconium, lanthanum, cerium, praseodymium, neodymium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, actinium, thorium, uranium, yttrium, gallium, magnesium, calcium, strontium, barium, cadmium, lithium, sodium, potassium, rubidium, and cesium.
15. The composition of claim 13 wherein E is an oxygen, chalcogenide and/or a halogen atom such as sulfur (also a glass former), selenium, tellurium and fluorine.
16. The composition of claim 13 wherein the preferred M is a main group glass former selected from the group consisting of boron, silicon, phosphorus, sulfur and metallic glass modifiers such as vanadium, titanium, zinc, lead, aluminum, zirconium, lanthanum, cerium, neodymium, magnesium, calcium, strontium, barium, lithium, sodium, and potassium atoms and E is an oxygen atom.
17. The composition of claim 1 wherein the most glass composition comprises the following formula:
[(P2O5)r1(Li2O)r2(B2O3)r3(A'O)r4(A"O)r5], wherein A' and A" are additional metallic glass modifiers, r1 is between 0.200 and 0.800, r2 is between 0.050 and 0.500, r3 is between 0.010 and 0.150, r4 is between 0.010 and 0.200, r5 is between 0.010 and 0.300, r1 + r2 + r3 + r4 + r5 = 1, and r1 > r2.
[(P2O5)r1(Li2O)r2(B2O3)r3(A'O)r4(A"O)r5], wherein A' and A" are additional metallic glass modifiers, r1 is between 0.200 and 0.800, r2 is between 0.050 and 0.500, r3 is between 0.010 and 0.150, r4 is between 0.010 and 0.200, r5 is between 0.010 and 0.300, r1 + r2 + r3 + r4 + r5 = 1, and r1 > r2.
18. The composition of claim 17 wherein A' and A" are selected from the group consisting of magnesium, barium, zinc and aluminum.
19. The composition of claim 1, wherein the filler comprises an oxide(s) selected from the group consisting of oxides of boron, aluminum, silicon, zinc, gallium, titanium, zirconium, manganese, iron, molybdenum, tungsten, bismuth, lead, lanthanum, cerium, neodymium, yttrium, calcium, magnesium and barium.
20. The composition of claim 1 wherein the clay filler comprises kaolin, calcined kaolin, mica, vermiculite and/or metakaolin.
21. The composition of claim 1, wherein said alkali silicate and/or alkali silicate precursors are present in an amount between 30 wt. % and 90 wt. % based upon the total composition.
22. The composition of claim 1, wherein said alkali silicate is formed from a alkali hydroxide and a SiO2 source and said alkali hydroxide is present in an amount of between 3 wt.
% to 40 wt. % and said SiO2 source is present in an amount of 15 wt. % to 75 wt. % based upon the total composition weight.
% to 40 wt. % and said SiO2 source is present in an amount of 15 wt. % to 75 wt. % based upon the total composition weight.
23. The composition of claim 1, wherein said reactive acidic glass is present in an amount of between 0.01 wt. % and 60 wt. % based upon the total composition.
24. The composition of claim 1, wherein said reactive acidic glass is present in an G:SiO2 ratio of between 0.01 and 50Ø
25. The composition of claim 1, wherein said clay filler is present in an amount of between 0.0 wt. % and 20 wt. % based upon the total composition weight.
26. The composition of claim 1, wherein said oxide filler is present in an amount of between 0.0 wt. % and 20 wt. % based upon the total composition weight.
27. The composition of claim 1 comprises the reaction product of the following:
a) 30 to 85 wt. % of alkali silicate;
b) 0.01 to 60 wt. % of a reactive acidic glass;
c) 0 to 20 wt. % of a clay filler d) 0 to 20 wt. % of an oxide; and e) 15 to 60 wt. % of water.
a) 30 to 85 wt. % of alkali silicate;
b) 0.01 to 60 wt. % of a reactive acidic glass;
c) 0 to 20 wt. % of a clay filler d) 0 to 20 wt. % of an oxide; and e) 15 to 60 wt. % of water.
28. The composition of claim 1 comprises the reaction product of the following:
a) 15 to 75 wt. % of a SiO2 source;
b) 3 to 40 wt. % of an alkali hydroxide;
c) 0.01 to 60 wt. % of a reactive acidic glass;
d) 0 to 20 wt. % of a clay filler;
e) 0 to 20 wt. % of an oxide; and f) 15 to 75 wt. % of water.
a) 15 to 75 wt. % of a SiO2 source;
b) 3 to 40 wt. % of an alkali hydroxide;
c) 0.01 to 60 wt. % of a reactive acidic glass;
d) 0 to 20 wt. % of a clay filler;
e) 0 to 20 wt. % of an oxide; and f) 15 to 75 wt. % of water.
29. A composition comprising the reaction product of water and the following mixture:
a) 20 to 99.9 wt. % of alkali silicate;
b) 0.01 to 80 wt. % of a reactive acidic glass;
c) 0 to 20 wt. % of a clay filler; and d) 0 to 20 wt. % of an oxide.
a) 20 to 99.9 wt. % of alkali silicate;
b) 0.01 to 80 wt. % of a reactive acidic glass;
c) 0 to 20 wt. % of a clay filler; and d) 0 to 20 wt. % of an oxide.
30. A composition comprising the reaction product of water and the following mixture:
a) 20 to 75 wt. % of SiO2 source;
b) 5 to 40 wt. % of alkali hydroxide;
c) 0.01 to 75 wt. % of a reactive acidic glass;
d) 0 to 20 wt. % of a clay filler; and e) 0 to 20 wt. % of an oxide.
a) 20 to 75 wt. % of SiO2 source;
b) 5 to 40 wt. % of alkali hydroxide;
c) 0.01 to 75 wt. % of a reactive acidic glass;
d) 0 to 20 wt. % of a clay filler; and e) 0 to 20 wt. % of an oxide.
31. The composition of claim 1 further includes non-clay filler materials.
32. The composition of claim 31, wherein the filler materials are selected from the group consisting of fibers, spheres, and particles.
33. The composition of claim 31, wherein the fibers are selected from a group consisting of continuous fibers and discontinuous fibers.
34. The composition of claim 31, wherein the spheres are selected from the group consisting of microspheres, macrospheres, hollow spheres, and solid spheres comprising glass, ceramic, metal, mineral, organic or inorganic materials.
35. The composition of claim 31, wherein the filler materials are utilized for reinforcement and selected from the group consisting of carbon fibers, glass fibers, alkali resistant glass fibers, mineral fibers, organic fibers, ceramic fibers and metallic fibers.
36. The composition of claim 35, wherein the reinforcement materials are selected from the group consisting of graphite fibers, E-glass fibers, S-glass fibers, basalt fibers, stainless steel fibers, titanium fibers, nickel alloy fibers, aramid fibers, polyethylene fibers, SiC fibers and BN
fibers.
fibers.
37. The inorganic matrix composition made from the composition of claim 1 and formed by curing the composition at a temperature ranging from 15°C to 1000°C (and higher) and a pressure range from vacuum (at ambient to 10-3 torr), and/or external pressure from ambient to 20,000 psi (137.895 MPa).
38. The inorganic matrix composition of claim 37 formed by curing the composition at 15°C to 200°C and an external pressure from ambient to 200 psi (1.378 MPa) and, alternatively, under vacuum (at ambient to 10-3 torr).
39. A method of making an inorganic silicate composite comprising the steps of applying an aqueous slurry of a mixture of an alkali silicate, a reactive acidic glass, water, and, optionally, a clay and/or oxide filler to a reinforcing medium and curing the composite by applying heat at a temperature of 15° C up to 1000°C and a pressure range from a vacuum from ambient to 10-3 torr, and/or external pressure from ambient to 20,000 psi (137.895 MPa).
40. The method of claim 39 wherein the uncured composite is in form of bulk molding compound, sheet molding compound, powder and reinforcement, liquid and reinforcement or prepreg.
41. The method of claim 39 wherein the composite is cured preferably at a temperature of 15°C up to 200°C and an external pressure from ambient to 200 psi (1.378 MPa), and optionally under a vacuum from ambient to 10-3 torr.
42. The method of claim 39 wherein the composite is cured using processes which include compression molding, pultrusion, wet layup, filament winding, autoclave vacuum bag processing, non-autoclave vacuum bag processing, vacuum infusion, liquid resin, film infusion or powder infusion, resin transfer molding, extrusion, injection molding, casting, spin casting, trapped elastomer molding and like processes.
43. The method of claim 39 wherein the composite is consolidated before and/or during the curing process.
44. The method of claim 39 wherein the slurry includes additional filler materials selected from the group consisting of carbon fibers, glass fibers, alkali resistant fibers, organic fibers, ceramic fibers, mineral fibers and metallic fibers.
45. The method of claim 39 wherein the slurry includes additional filler materials selected from the group consisting of graphite fibers, E-glass fibers, S-glass fibers, stainless steel fibers, titanium fibers, nickel alloy fibers, aramid fibers, polyethylene fibers, basalt fibers, SiC
fibers and BN fibers.
fibers and BN fibers.
46. The method of claim 39 wherein the reinforcing medium is a glass fiber such as an E-glass fiber, S-glass fiber and/or an alkaline resistant fiber.
47. An alkali silicate slurry composition for forming an inorganic polymer network comprising an alkali silicate or a mixture that yields an insitu alkali silicate, a reactive acidic glass, water and optionally a modifier that moderates the gelation of matrix binder suspension and/or a clay and/or oxide filler to enhance physical and thermal properties.
48. The composition of claim 47, wherein the gel modifier is an organic acid or organic base.
49. The composition of claim 47, wherein said organic acid is an .alpha.-hydroxyacid and/or a .beta.-hydroxyacid.
50. The composition of claim 47, wherein said organic base is substituted nitrogen organic base.
51. The composition of claim 47, wherein said organic base is a substituted pyridine.
52. The composition of claim 47, wherein said organic base is quinoline.
53. The composition of claim 47, wherein said gel modifier is present in an amount of between 0.0 wt. % and 10 wt. % based upon the total composition.
54. A method of making an inorganic silicate composite comprising the steps of applying an aqueous slurry of a mixture of an alkali silicate, a reactive acidic glass, water and optionally a modifier that moderates the gelation of matrix binder suspension and/or a clay and/or oxide filler to a reinforcing medium and curing the composite by applying heat at a temperature of 15° C up to 1000°C and pressures under vacuum (ambient to 10-3 torr, e.g.
vacuum bagging) and/or external pressure from ambient to 20,000 psi (137.895 MPa).
vacuum bagging) and/or external pressure from ambient to 20,000 psi (137.895 MPa).
Applications Claiming Priority (5)
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| US09/871,998 | 2001-06-01 | ||
| US09/871,998 US6969422B2 (en) | 2000-09-20 | 2001-06-01 | Inorganic matrix composition and composites incorporating the matrix composition |
| PCT/US2001/029375 WO2002024596A2 (en) | 2000-09-20 | 2001-09-18 | Inorganic matrix compositions and composites incorporating the matrix composition |
Publications (1)
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|---|---|
| CA2425179A1 true CA2425179A1 (en) | 2002-03-28 |
Family
ID=26927438
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|---|---|---|---|
| CA002425179A Abandoned CA2425179A1 (en) | 2000-09-20 | 2001-09-18 | Inorganic matrix compositions and composites incorporating the matrix composition |
Country Status (10)
| Country | Link |
|---|---|
| US (2) | US6969422B2 (en) |
| EP (1) | EP1328489A2 (en) |
| CN (1) | CN1254451C (en) |
| AU (1) | AU2001292840A1 (en) |
| CA (1) | CA2425179A1 (en) |
| IL (2) | IL155721A0 (en) |
| MX (1) | MXPA03003460A (en) |
| NO (1) | NO20033100L (en) |
| NZ (1) | NZ525404A (en) |
| WO (1) | WO2002024596A2 (en) |
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| US20260103426A1 (en) * | 2023-07-11 | 2026-04-16 | A&A Green Phoenix Group Joint Stock Company | Process for producing a hot blended material of amorphous silicon dioxide – crystalline silicon dioxide, process for producing artificial stone from the material by press-vibration method in vacuum environment and the artificial stone product obtained from this process |
| CN119500969B (en) * | 2024-09-20 | 2026-04-21 | 潍柴动力股份有限公司 | Sand casting coating capable of preventing gray cast iron nitrogen holes from being generated and preparation method thereof |
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- 2001-06-01 US US09/871,998 patent/US6969422B2/en not_active Expired - Lifetime
- 2001-09-18 EP EP01973239A patent/EP1328489A2/en not_active Withdrawn
- 2001-09-18 CN CNB018191983A patent/CN1254451C/en not_active Expired - Fee Related
- 2001-09-18 IL IL15572101A patent/IL155721A0/en active IP Right Grant
- 2001-09-18 WO PCT/US2001/029375 patent/WO2002024596A2/en not_active Ceased
- 2001-09-18 NZ NZ525404A patent/NZ525404A/en unknown
- 2001-09-18 AU AU2001292840A patent/AU2001292840A1/en not_active Abandoned
- 2001-09-18 MX MXPA03003460A patent/MXPA03003460A/en not_active Application Discontinuation
- 2001-09-18 CA CA002425179A patent/CA2425179A1/en not_active Abandoned
-
2003
- 2003-05-01 IL IL155721A patent/IL155721A/en not_active IP Right Cessation
- 2003-07-07 NO NO20033100A patent/NO20033100L/en unknown
-
2004
- 2004-07-21 US US10/897,298 patent/US6986859B2/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101956433A (en) * | 2010-09-13 | 2011-01-26 | 天津安美环境科技工程有限公司 | Expanded perlite fire-proof composite core plate |
| CN101956433B (en) * | 2010-09-13 | 2014-05-07 | 天津安美环境科技工程有限公司 | Expanded perlite fire-proof composite core plate preparation process |
Also Published As
| Publication number | Publication date |
|---|---|
| NO20033100D0 (en) | 2003-07-07 |
| IL155721A0 (en) | 2003-11-23 |
| WO2002024596A3 (en) | 2002-06-20 |
| IL155721A (en) | 2006-08-20 |
| AU2001292840A1 (en) | 2002-04-02 |
| EP1328489A2 (en) | 2003-07-23 |
| WO2002024596A2 (en) | 2002-03-28 |
| US6986859B2 (en) | 2006-01-17 |
| US20050003947A1 (en) | 2005-01-06 |
| US20020058576A1 (en) | 2002-05-16 |
| MXPA03003460A (en) | 2004-12-06 |
| CN1254451C (en) | 2006-05-03 |
| NZ525404A (en) | 2005-11-25 |
| US6969422B2 (en) | 2005-11-29 |
| CN1474790A (en) | 2004-02-11 |
| NO20033100L (en) | 2003-07-07 |
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| EEER | Examination request | ||
| FZDE | Discontinued |